Publications of Earl H. Dowell    :chronological  alphabetical  combined  bibtex listing:

Papers Published

1. Dowell, E, Reduced-order modeling: a personal journey, Nonlinear Dynamics, vol. 111 no. 11 (June, 2023), pp. 9699-9720 [doi]  [abs]
2. Wayhs-Lopes, LD; Dowell, EH; Bueno, DD, A new look at the Equivalent Linearization Technique to predict LCO in aeroelastic systems with discrete nonlinearities, Journal of Fluids and Structures, vol. 119 (May, 2023) [doi]  [abs]
3. Cheng, Z; Lien, FS; Dowell, EH; Yee, E, Triggering of galloping in structures at low Reynolds numbers, Journal of Fluids and Structures, vol. 118 (April, 2023) [doi]  [abs]
4. Li, C; Pan, T; Yan, Z; Zheng, M; Li, Q; Dowell, EH, Aerodynamic Characteristics of Morphing Supersonic Cascade Under Low-Upstream-Mach-Number Condition, Aiaa Journal, vol. 61 no. 4 (April, 2023), pp. 1708-1719 [doi]  [abs]
5. Latif, U; Dowell, EH; Uddin, E; Yamin Younis, M, Parametric aerodynamic and aeroelastic study of a deformable flag-based energy harvester for powering low energy devices, Energy Conversion and Management, vol. 280 (March, 2023) [doi]  [abs]
6. Thomas, JP; Dowell, EH, Methodology for Numerically Stabilizing a Harmonic-Balance-Based Forced Response Aeroelastic Solution Approach, Aiaa Journal, vol. 61 no. 2 (February, 2023), pp. 965-972 [doi]
7. Modaress-Aval, AH; Bakhtiari-Nejad, F; Dowell, EH; Shahverdi, H; Peters, D, Comparative Study of Beam and Plate Theories for Moderate Aspect Ratio Wings, Aiaa Journal, vol. 61 no. 2 (February, 2023), pp. 859-874 [doi]  [abs]
8. Geronel, RS; Dowell, EH; Bueno, DD, Estimating the oscillation frequency of a payload mass on quadcopter in non-autonomous flight, Journal of Vibration and Control, vol. 29 no. 1-2 (January, 2023), pp. 236-250 [doi]  [abs]
9. Brown, C; McGowan, G; Cooley, K; Deese, J; Josey, T; Dowell, EH; Thomas, JP, Convolution/Volterra Reduced-Order Modeling for Nonlinear Aeroelastic Limit Cycle Oscillation Analysis and Control, Aiaa Journal, vol. 60 no. 12 (December, 2022), pp. 6647-6664 [doi]  [abs]
10. Cheng, Z; Lien, FS; Dowell, EH; Wang, R; Zhang, JH, Data-driven stability analysis via the superposition of reduced-order models for the flutter of circular cylinder submerged in three-dimensional spanwise shear inflow at subcritical Reynolds number, Physics of Fluids, vol. 34 no. 12 (December, 2022) [doi]  [abs]
11. He, Y; Shi, A; Dowell, EH; Li, X, Panel Aeroelastic Stability in Irregular Shock Reflection, Aiaa Journal, vol. 60 no. 11 (November, 2022), pp. 6490-6499 [doi]
12. Freydin, M; Dowell, EH; Varigonda, SV; Narayanaswamy, V, Response of a plate with piezoelectric elements to turbulent pressure fluctuation in supersonic flow, Journal of Fluids and Structures, vol. 114 (October, 2022) [doi]  [abs]
13. Serafim, LP; Werner, E; Zhou, J; Dowell, EH, Static and Dynamic Nonlinear In-Plane Effect in the Response of a Cantilevered Plate With Tip Mass Load: Theory and Experiment, Journal of Applied Mechanics, vol. 89 no. 10 (October, 2022) [doi]  [abs]
14. Qin, Z; Shi, A; Dowell, EH; Pei, Y; Huang, E, Analytical Model of Strong Mach Reflection, Aiaa Journal, vol. 60 no. 9 (September, 2022), pp. 5187-5202 [doi]  [abs]
15. Deliyianni, M; McHugh, K; Webster, JT; Dowell, E, Dynamic equations of motion for inextensible beams and plates, Archive of Applied Mechanics, vol. 92 no. 6 (June, 2022), pp. 1929-1952 [doi]  [abs]
16. Dowell, EH, Preface to the second edition, vol. 264 (January, 2022), pp. xiii
17. Dowell, EH, Preface to the third edition, vol. 264 (January, 2022), pp. xi
18. Dowell, EH, Preface to the fourth edition, vol. 264 (January, 2022), pp. ix
19. Dowell, EH, Preface to the fifth edition, vol. 264 (January, 2022), pp. vii
20. Dowell, EH, Preface to the sixth edition, vol. 264 (January, 2022), pp. v-vi
21. Dowell, EH, Preface to the first edition, vol. 264 (January, 2022), pp. xv-xvi
22. Brown, C; McGowan, G; Cooley, K; Deese, J; Josey, T; Dowell, EH; Thomas, JP, Convolution/Volterra Reduced-Order Modeling for Flutter and LCO Predictions in Highly Nonlinear Systems, Aiaa Science and Technology Forum and Exposition, Aiaa Scitech Forum 2022 (January, 2022), ISBN 9781624106316 [doi]  [abs]
23. Levin, D; Bastos, KK; Dowell, EH, Convolution and Volterra Series Approach to Reduced-Order Modeling of Unsteady Aerodynamic Loads, Aiaa Journal, vol. 60 no. 3 (January, 2022), pp. 1663-1678 [doi]  [abs]
24. Bueno, DD; Wayhs-Lopes, LD; Dowell, EH, Control-Surface Structural Nonlinearities in Aeroelasticity: A State of the Art Review, Aiaa Journal, vol. 60 no. 6 (January, 2022), pp. 3364-3376 [doi]  [abs]
25. Thomas, JP; Dowell, EH, Non-Intrusive Polynomial Chaos Approach for Nonlinear Aeroelastic Uncertainty Quantification, Aiaa Aviation 2022 Forum (January, 2022), ISBN 9781624106354 [doi]  [abs]
26. McHugh, K; Beran, P; Dowell, E, COMPUTATIONAL STUDY OF CANTILEVERED PLATE IN HIGH SPEED AXIAL FLOW, Proceedings of the International Forum of Aeroelasticity and Structural Dynamics 2022, Ifasd 2022 (January, 2022), ISBN 9788409423538  [abs]
27. Padmanabhan, MA; Dowell, EH, Computational study of aeroelastic response due to freeplay and flight loads, Aiaa Journal, vol. 59 no. 7 (July, 2021), pp. 2793-2799 [doi]
28. Freydin, M; Dowell, EH, Fully coupled nonlinear aerothermoelastic computational model of a plate in hypersonic flow, Aiaa Journal, vol. 59 no. 7 (July, 2021), pp. 2725-2736 [doi]  [abs]
29. Bueno, DD; Dowell, EH, A note on the state space representation of aeroelastic systems for time domain analysis, Journal of Fluids and Structures, vol. 104 (July, 2021) [doi]  [abs]
30. Abad, MJS; Mahmoudi, M; Dowell, E, Novel technique for dynamic analysis of shear frames based on energy balance equations, Scientia Iranica, vol. 27 no. 3A (May, 2021), pp. 1091-1112 [doi]  [abs]
31. Zhou, JW; Zhang, W; Wang, XS; Mann, BP; Dowell, EH, Primary resonance suppression of a base excited oscillator using a spatially constrained system: Theory and experiment, Journal of Sound and Vibration, vol. 496 (March, 2021) [doi]  [abs]
32. Freydin, M; Dowell, EH; Spottswood, SM; Perez, RA, Nonlinear dynamics and flutter of plate and cavity in response to supersonic wind tunnel start, Nonlinear Dynamics, vol. 103 no. 4 (March, 2021), pp. 3019-3036 [doi]  [abs]
33. Schöneich, AG; Whalen, TJ; Laurence, SJ; Sullivan, BT; Bodony, DJ; Freydin, M; Dowell, EH; Stacey, LJ; Buck, GM, Fluid-thermal-structural interactions in ramp-induced shock-wave/boundary-layer interactions at mach 6, Aiaa Scitech 2021 Forum (January, 2021), pp. 1-13, ISBN 9781624106095  [abs]
34. Thomas, JP; Dowell, EH, Automatic differentiation based nonlinear reduced-order model with geometric gradient computation capability, Aiaa Scitech 2021 Forum (January, 2021), pp. 1-17, ISBN 9781624106095  [abs]
35. Freydin, M; Dowell, EH, Nonlinear theoretical aeroelastic model of a plate: Free to fixed in-plane boundaries, Aiaa Journal, vol. 59 no. 2 (January, 2021), pp. 658-672 [doi]  [abs]
36. Ribeiro, FA; Dowell, EH; Bueno, DD, Enhancement to least square-based approach for time-domain unsteady aerodynamic approximation, Journal of Aircraft, vol. 58 no. 1 (January, 2021), pp. 111-124 [doi]  [abs]
37. McHugh, KA; Freydin, M; Bastos, KK; Beran, P; Dowell, EH, Flutter and limit cycle oscillations of cantilevered plate in supersonic flow, Journal of Aircraft, vol. 58 no. 2 (January, 2021), pp. 266-278 [doi]  [abs]
38. Bueno, DD; Gonsalez Bueno, CG; Dowell, EH, A modal approach for designing controllers for active flutter suppression, Journal of the Brazilian Society of Mechanical Sciences and Engineering, vol. 43 no. 1 (January, 2021) [doi]  [abs]
39. Shi, A; Dowell, EH, A Benchmark Method for Predicting Oblique Shock Structure, 32nd Congress of the International Council of the Aeronautical Sciences, Icas 2021 (January, 2021), ISBN 9783932182914  [abs]
40. Thomas, JP; Dowell, EH, Nonlinear Aeroelastic Reduced-Order Modeling Approach with Geometric Gradient Computation Capability, Aiaa Aviation and Aeronautics Forum and Exposition, Aiaa Aviation Forum 2021 (January, 2021), ISBN 9781624106101 [doi]  [abs]
41. Lee, MW; Dowell, EH, Improving the predictable accuracy of fluid Galerkin reduced-order models using two POD bases, Nonlinear Dynamics, vol. 101 no. 2 (July, 2020), pp. 1457-1471 [doi]  [abs]
42. Modaress-Aval, AH; Bakhtiari-Nejad, F; Dowell, EH; Shahverdi, H; Rostami, H; Peters, DA, Aeroelastic analysis of cantilever plates using Peters’ aerodynamic model, and the influence of choosing beam or plate theories as the structural model, Journal of Fluids and Structures, vol. 96 (July, 2020) [doi]  [abs]
43. Wayhs-Lopes, LD; Dowell, EH; Bueno, DD, Influence of friction and asymmetric freeplay on the limit cycle oscillation in aeroelastic system: An extended Hénon's technique to temporal integration, Journal of Fluids and Structures, vol. 96 (July, 2020) [doi]  [abs]
44. Shi, A; Chen, J; Dowell, EH; Wen, H; Li, X; Shen, T, Relativistic oblique shock: A geometric object, The Astrophysical Journal, vol. 893 no. 2 (April, 2020) [doi]  [abs]
45. Rodrigues, DL; Dowell, EH; Bueno, DD, On the stiffness and damping characteristics of magnetorheological dampers and their implications for flutter analysis, Engineering Research Express, vol. 2 no. 1 (March, 2020) [doi]  [abs]
46. McHugh, KA; Dowell, EH, Nonlinear Response of an Inextensible, Free-Free Beam Subjected to a Nonconservative Follower Force, Journal of Computational and Nonlinear Dynamics, vol. 15 no. 2 (February, 2020) [doi]  [abs]
47. Freydin, M; Dowell, EH; Whalen, TJ; Laurence, SJ, A theoretical computational model of a plate in hypersonic flow, Journal of Fluids and Structures, vol. 93 (February, 2020) [doi]  [abs]
48. Shi, A; Chen, J; Dowell, EH; Wen, H, Approach to determine the most efficient supersonic mach number, Aiaa Journal, vol. 58 no. 3 (January, 2020), pp. 1402-1406 [doi]
49. Ma, Z; Lei, L; Dowell, E; Zeng, P, An experimental study on the actuator line method with anisotropic regularization kernel, Energies, vol. 13 no. 4 (January, 2020) [doi]  [abs]
50. Amirzadegan, S; Dowell, EH, Nonlinear limit cycle oscillation and flutter analysis of clamped curved plates, Journal of Aircraft, vol. 57 no. 2 (January, 2020), pp. 368-376 [doi]  [abs]
51. Padmanabhan, MA; Dowell, EH, Gust response computations with control surface freeplay using random input describing functions, Aiaa Journal, vol. 58 no. 7 (January, 2020), pp. 2899-2908 [doi]  [abs]
52. Whalen, TJ; Schöneich, AG; Laurence, SJ; Sullivan, BT; Bodony, DJ; Freydin, M; Dowell, EH; Buck, GM, Hypersonic fluid–structure interactions in compression corner shock-wave/boundary-layer interaction, Aiaa Journal, vol. 58 no. 9 (January, 2020), pp. 4090-4105 [doi]  [abs]
53. Thomas, JP; Dowell, EH, Methodology for numerically stabilizing a harmonic balance based aeroelastic solution approach, Aiaa Scitech 2020 Forum, vol. 1 PartF (January, 2020), ISBN 9781624105951 [doi]  [abs]
54. Lee, MW; Dowell, EH, On the importance of numerical error in constructing pod-based reduced-order models of nonlinear fluid flows, Aiaa Scitech 2020 Forum (January, 2020), pp. 1-14, ISBN 9781624105951 [doi]  [abs]
55. Thomas, JP; Dowell, EH, Discrete adjoint constrained design optimization approach for unsteady transonic aeroelasticity and buffet, Aiaa Aviation 2020 Forum, vol. 1 PartF (January, 2020), pp. 1-13, ISBN 9781624105982 [doi]  [abs]
56. Freydin, M; Levin, D; Dowell, EH; Varigonda, SV; Narayanaswamy, V, Natural frequencies of a heated plate: Theory and experiment, Aiaa Journal, vol. 58 no. 11 (January, 2020), pp. 4969-4973 [doi]  [abs]
57. Bueno, DD; Dowell, EH, Revisiting the fundamentals of control surface reversal including nonlinear effects, Journal of Aircraft, vol. 57 no. 6 (January, 2020), pp. 1212-1219 [doi]  [abs]
58. Zhou, T; Dowell, E; Feng, SS, Computational investigation of wind tunnel wall effects on buffeting flow and lock-in for an airfoil at high angle of attack, Aerospace Science and Technology, vol. 95 (December, 2019) [doi]  [abs]
59. Culver, D; McHugh, K; Dowell, E, An assessment and extension of geometrically nonlinear beam theories, Mechanical Systems and Signal Processing, vol. 134 (December, 2019) [doi]  [abs]
60. Ding, H; Huang, LL; Dowell, E; Chen, LQ, Stress distribution and fatigue life of nonlinear vibration of an axially moving beam, Science China Technological Sciences, vol. 62 no. 7 (July, 2019), pp. 1123-1133 [doi]  [abs]
61. Lee, MW; Dowell, EH; Balajewicz, MJ, A study of the regularized lid-driven cavity's progression to chaos, Communications in Nonlinear Science and Numerical Simulation, vol. 71 (June, 2019), pp. 50-72 [doi]  [abs]
62. Tang, DM; Levin, D; Dowell, EH, Experimental and theoretical correlations for energy harvesting from a large flapping flag response, Journal of Fluids and Structures, vol. 86 (April, 2019), pp. 290-315 [doi]  [abs]
63. McHugh, KA; Dowell, EH, Nonlinear Response of an Inextensible, Cantilevered Beam Subjected to a Nonconservative Follower Force, Journal of Computational and Nonlinear Dynamics, vol. 14 no. 3 (March, 2019) [doi]  [abs]
64. Wei, Y; Dowell, EH; Chen, Z, Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal, International Journal of Turbo and Jet Engines, vol. 36 no. 1 (March, 2019), pp. 31-43 [doi]  [abs]
65. Modaress-Aval, AH; Bakhtiari-Nejad, F; Dowell, EH; Peters, DA; Shahverdi, H, A comparative study of nonlinear aeroelastic models for high aspect ratio wings, Journal of Fluids and Structures, vol. 85 (February, 2019), pp. 249-274 [doi]  [abs]
66. Raviv Sayag, M; Dowell, EH, Nonlinear structural, inertial and damping effects in an oscillating cantilever beam, Conference Proceedings of the Society for Experimental Mechanics Series, vol. 1 (January, 2019), pp. 387-400, ISBN 9783319742793 [doi]  [abs]
67. Doherty, J; Joshi, M; Levin, D; Rauseo, M; Sharma, M; Kielb, R; Dowell, E, Nonlinear interaction of a flutter induced limit cycle oscillation of a cantilevered wing with a forced gust excitation, Aiaa Scitech 2019 Forum (January, 2019), ISBN 9781624105784 [doi]  [abs]
68. Poplingher, L; Raveh, DE; Dowell, EH, Modal analysis of transonic shock buffet on 2D airfoil, Aiaa Journal, vol. 57 no. 7 (January, 2019), pp. 2851-2866 [doi]  [abs]
69. Amirzadegan, S; Dowell, EH, Correlation of experimental and computational results for flutter of streamwise curved plate, Aiaa Journal, vol. 57 no. 8 (January, 2019), pp. 3556-3561 [doi]  [abs]
70. Wen, H; Shi, A; Dowell, EH; Li, X, Measuring the Aero-Refueling Hose Model’s Sectional-Bending-Stiffness in the RMCFLM Experimental System, Lecture Notes in Electrical Engineering, vol. 459 (January, 2019), pp. 2974-2991, ISBN 9789811333040 [doi]  [abs]
71. McHugh, KA; Beran, P; Freydin, M; Dowell, E, Flutter and limit cycle oscillations of a cantilevered plate in supersonic/hypersonic flow, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
72. Kim, T; Thomas, JP; Dowell, EH, Flutter prediction based on dynamic eigen decomposition of coupled CFD-CSD flight simulation, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
73. Kruger Bastos, KM; Dowell, EH, RANS and DNS study of buffet in subsonic and transonic flow, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
74. Freydin, M; Dowell, EH; Currao, GMD; Neely, AJ, Computational study for the design of a hypersonic panel flutter experiment, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
75. Levin, D; Dowell, EH, Improving piezoelectric energy harvesting from an aeroelastic system, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
76. McHugh, KA; Beran, P; Freydin, M; Dowell, E, Flutter and limit cycle oscillations of a cantilevered plate in supersonic/hypersonic flow, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
77. Kim, T; Thomas, JP; Dowell, EH, Flutter prediction based on dynamic eigen decomposition of coupled CFD-CSD flight simulation, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
78. Kruger Bastos, KM; Dowell, EH, RANS and DNS study of buffet in subsonic and transonic flow, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
79. Levin, D; Dowell, EH, Improving piezoelectric energy harvesting from an aeroelastic system, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
80. Freydin, M; Dowell, EH; Currao, GMD; Neely, AJ, Computational study for the design of a hypersonic panel flutter experiment, International Forum on Aeroelasticity and Structural Dynamics 2019, Ifasd 2019 (January, 2019)  [abs]
81. Shi, A; Wen, H; Dowell, EH; Chen, J, A new approach to determine the most efficient supersonic mach number, Aiaa Aviation 2019 Forum (January, 2019), pp. 1-9, ISBN 9781624105890 [doi]  [abs]
82. Thomas, JP; Dowell, EH, Discrete adjoint approach for nonlinear unsteady aeroelastic design optimization, Aiaa Journal, vol. 57 no. 10 (January, 2019), pp. 4368-4376 [doi]  [abs]
83. Shi, A; Dowell, EH, Theoretical solutions and physical significances for minimum ratio of total pressure loss by oblique shock, Hangkong Xuebao/Acta Aeronautica Et Astronautica Sinica, vol. 39 no. 12 (December, 2018) [doi]  [abs]
84. Zhang, W; Wu, QL; Yao, MH; Dowell, EH, Analysis on global and chaotic dynamics of nonlinear wave equations for truss core sandwich plate, Nonlinear Dynamics, vol. 94 no. 1 (October, 2018), pp. 21-37, Springer Nature America, Inc [doi]  [abs]
85. Askarian, AR; Abtahi, H; Firouz-Abadi, RD; Haddadpour, H; Dowell, EH, Bending-torsional instability of a viscoelastic cantilevered pipe conveying pulsating fluid with an inclined terminal nozzle, Journal of Mechanical Science and Technology, vol. 32 no. 7 (July, 2018), pp. 2999-3008, Springer Nature America, Inc [doi]  [abs]
86. Kasem, MM; Dowell, EH, A study of the natural modes of vibration and aeroelastic stability of a plate with a piezoelectric material, Smart Materials and Structures, vol. 27 no. 7 (June, 2018), pp. 075043-075043, IOP Publishing [doi]  [abs]
87. Wu, QL; Zhang, W; Dowell, EH, Detecting multi-pulse chaotic dynamics of high-dimensional non-autonomous nonlinear system for circular mesh antenna, International Journal of Non Linear Mechanics, vol. 102 (June, 2018), pp. 25-40, Elsevier BV [doi]  [abs]
88. Ding, H; Dowell, EH; Chen, LQ, Transmissibility of Bending Vibration of an Elastic Beam, Journal of Vibration and Acoustics, vol. 140 no. 3 (June, 2018), pp. 031007-031007, ASME International [doi]  [abs]
89. Wei, Y; Chen, Z; Dowell, EH, Nonlinear Characteristics Analysis of a Rotor-Bearing-Brush Seal System, International Journal of Structural Stability and Dynamics, vol. 18 no. 5 (May, 2018), pp. 1850063-1850063 [doi]  [abs]
90. McHugh, K; Dowell, E, Nonlinear Responses of Inextensible Cantilever and Free-Free Beams Undergoing Large Deflections, Journal of Applied Mechanics, vol. 85 no. 5 (May, 2018), pp. 051008-051008, ASME International [doi]  [abs]
91. Wang, Z-H; Belyaev, IV; Zhang, X-Z; Bi, C-X; Faranosov, GA; Dowell, EH, The sound field of a rotating dipole in a plug flow., The Journal of the Acoustical Society of America, vol. 143 no. 4 (April, 2018), pp. 2099 [doi]  [abs]
92. Culver, D; Dowell, E, On modal cross-coupling in the asymptotic modal limit, Journal of Sound and Vibration, vol. 416 (March, 2018), pp. 172-191, Elsevier BV [doi]  [abs]
93. Culver, D; Dowell, E, Iterative techniques for analyzing nonlinear vibrating dynamical systems in the frequency domain, Nonlinear Dynamics, vol. 91 no. 4 (March, 2018), pp. 2113-2140, Springer Nature [doi]  [abs]
94. Zhou, T; Feng, SS; Dowell, EH, Buffeting and lock in of an airfoil at high angle of attack, Journal of Aircraft, vol. 55 no. 2 (January, 2018), pp. 771-780, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
95. Moradi, M; Sadeghi, MH; Dowell, EH, Engineering notes experimental and theoretical flutter investigation for a range of wing wind-tunnel models, Journal of Aircraft, vol. 55 no. 2 (January, 2018), pp. 891-896, American Institute of Aeronautics and Astronautics (AIAA) [doi]
96. Thomas, JP; Dowell, EH, A fixed point iteration approach for harmonic balance based aeroelastic computations, Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference, 2018 no. 210049 (January, 2018), ISBN 9781624105326 [doi]  [abs]
97. Kim, T; Dowell, EH, Flutter prediction based on dynamic eigen decomposition of flight data with limited actuators and sensors, Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference, 2018 no. 210049 (January, 2018), American Institute of Aeronautics and Astronautics, ISBN 9781624105326 [doi]  [abs]
98. Li, Z; Zhang, P; Pan, T; Li, Q; Zhang, J; Dowell, EH, Catastrophe-theory-based modeling of airfoil-stall boundary at low reynolds numbers, Aiaa Journal, vol. 56 no. 1 (January, 2018), pp. 36-45, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
99. Padmanabhan, MA; Dowell, EH; Pasiliao, CL, Computational study of aeroelastic limit cycles due to localized structural nonlinearities, Journal of Aircraft, vol. 55 no. 4 (January, 2018), pp. 1531-1541, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
100. Thomas, JP; Dowell, EH; Anderson, M; McGowan, GZ, Progress toward efficient compression algorithms for application in flight simulation environments, 2018 Modeling and Simulation Technologies Conference, vol. 16 no. 7 (January, 2018), pp. 278-288, American Institute of Aeronautics and Astronautics, ISBN 9781624105517 [doi]  [abs]
101. Tang, DM; Dowell, EH, Aeroelastic response and energy harvesting from a cantilevered piezoelectric laminated plate, Journal of Fluids and Structures, vol. 76 (January, 2018), pp. 14-36, Elsevier BV [doi]  [abs]
102. McHugh, KA; Dowell, EH, Nonlinear response of an inextensible, cantilevered beam subjected to a nonconservative follower force, Proceedings of the Asme Design Engineering Technical Conference, vol. 6 (January, 2018), ASME, ISBN 9780791851838 [doi]  [abs]
103. Currao, GMD; Freydin, M; Dowell, E; McQuellin, LP; Neely, AJ, Design of a panel flutter experiment in a short duration hypersonic facility, Proceedings of the 21st Australasian Fluid Mechanics Conference, Afmc 2018 (January, 2018), ISBN 9780646597843  [abs]
104. Currao, GMD; Freydin, M; Dowell, E; McQuellin, LP; Neely, AJ, Design of a panel flutter experiment in a short duration hypersonic facility, Proceedings of the 21st Australasian Fluid Mechanics Conference, Afmc 2018 (January, 2018), ISBN 9780646597843  [abs]
105. Currao, GMD; Freydin, M; Dowell, E; McQuellin, LP; Neely, AJ, Design of a panel flutter experiment in a short duration hypersonic facility, Proceedings of the 21st Australasian Fluid Mechanics Conference, Afmc 2018 (January, 2018), ISBN 9780646597843  [abs]
106. Ding, H; Tan, X; Dowell, EH, Natural frequencies of a super-critical transporting Timoshenko beam, European Journal of Mechanics A/Solids, vol. 66 (November, 2017), pp. 79-93, Elsevier BV [doi]  [abs]
107. Culver, DR; Dowell, EH, High Frequency Analysis of a Point-Coupled Parallel Plate System, Journal of Vibration and Acoustics, vol. 139 no. 5 (October, 2017), pp. 051002-051002 [doi]  [abs]
108. Ganji, HF; Dowell, EH, Sound transmission and radiation from a plate-cavity system in supersonic flow, Journal of Aircraft, vol. 54 no. 5 (September, 2017), pp. 1877-1900, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
109. Mannarino, A; Dowell, EH; Mantegazza, P, An adaptive controller for nonlinear flutter suppression and free-play compensation, Journal of Vibration and Control, vol. 23 no. 14 (August, 2017), pp. 2269-2290, SAGE Publications [doi]  [abs]
110. Pasolini, P; Dowell, EH; De Rosa, S; Franco, F; Savino, R, Non-linear aero-elastic response of a multi-layer TPS, Advances in Aircraft and Spacecraft Science, vol. 4 no. 4 (July, 2017), pp. 449-465 [doi]  [abs]
111. Wei, Y; Dowell, EH; Chen, Z; Jiao, Y; Zhang, Z, Influence of Geometry on Rotordynamic Coefficients of Brush Seal, International Journal of Turbo and Jet Engines, vol. 34 no. 2 (May, 2017), pp. 155-166 [doi]  [abs]
112. Dowell, E, Hamilton’s principle and Hamilton’s equations with holonomic and non-holonomic constraints, Nonlinear Dynamics, vol. 88 no. 2 (April, 2017), pp. 1093-1097, Springer Nature [doi]  [abs]
113. Eugeni, M; Mastroddi, F; Dowell, EH, Normal form analysis of a forced aeroelastic plate, Journal of Sound and Vibration, vol. 390 (March, 2017), pp. 141-163, Elsevier BV [doi]  [abs]
114. Verstraelen, E; Dimitriadis, G; Rossetto, GDB; Dowell, EH, Two-domain and three-domain limit cycles in a typical aeroelastic system with freeplay in pitch, Journal of Fluids and Structures, vol. 69 (February, 2017), pp. 89-107, Elsevier BV [doi]  [abs]
115. Culver, DR; Dowell, E, High frequency analysis of a dynamically coupled parallel plate system, Asme 2017 Dynamic Systems and Control Conference, Dscc 2017, vol. 3 (January, 2017), ASME, ISBN 9780791858295 [doi]  [abs]
116. McHugh, K; Dowell, E, Nonlinear responses of inextensible cantilever and free-free beams undergoing large deflections, Asme 2017 Dynamic Systems and Control Conference, Dscc 2017, vol. 3 (January, 2017), ASME, ISBN 9780791858295 [doi]  [abs]
117. Padmanabhan, MA; Dowell, EH, Calculation of aeroelastic limit cycles due to localized nonlinearity and static preload, Aiaa Journal, vol. 55 no. 8 (January, 2017), pp. 2762-2772, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
118. Abad, MJS; Mahmoudi, M; Dowell, EH, Dynamic analysis of SDOF systems using modified energy method, Asian Journal of Civil Engineering, vol. 18 no. 7 (January, 2017), pp. 1125-1146  [abs]
119. Kim, T; Dowell, EH, Parametrically rich nonlinear reduced-order modeling: An application in viscous incompressible flow, 17th International Forum on Aeroelasticity and Structural Dynamics, Ifasd 2017, vol. 2017-June (January, 2017), ISBN 9788897576280  [abs]
120. Dowell, EH; Williams, MH; Chi, MR, ASSESSMENT OF THEORETICAL MODELS FOR VISCOUS AND TRANSONIC FLOW., Agard Conference Proceedings (January, 2017)  [abs]
121. Al-Mashhadani, WJ; Dowell, EH; Wasmi, HR; Al-Asadi, AA, Aeroelastic response and limit cycle oscillations for wing-flap-tab section with freeplay in tab, Journal of Fluids and Structures, vol. 68 (January, 2017), pp. 403-422, Elsevier BV [doi]  [abs]
122. Shi, A; Jiang, L; Dowell, EH; Qin, Z, A novel experimental mechanics method for measuring the light pressure acting on a solar sail membrane, Smart Structures and Materials 2005: Active Materials: Behavior and Mechanics, vol. 10256 (January, 2017), SPIE [doi]  [abs]
123. Bakhtiari-Nejad, F; Modarres, AH; Dowell, EH; Shahverdi, H, Linear and nonlinear aeroelastic analysis of a high aspect ratio wing, Proceedings of the Asme Design Engineering Technical Conference, vol. 8 (January, 2017), ASME, ISBN 9780791858226 [doi]  [abs]
124. Dowell, E, Modal damping in a finite element model (L), The Journal of the Acoustical Society of America, vol. 140 no. 4 (October, 2016), pp. 2288-2289, Acoustical Society of America (ASA) [doi]  [abs]
125. Sayag, MR; Dowell, EH, Linear Versus Nonlinear Response of a Cantilevered Beam under Harmonic Base Excitation: Theory and Experiment, Journal of Applied Mechanics, vol. 83 no. 10 (October, 2016), pp. 101002-101002, ASME International [doi]  [abs]
126. Culver, D; Dowell, E, High frequency analysis of a plate carrying a concentrated nonlinear spring–mass system, Journal of Sound and Vibration, vol. 379 (September, 2016), pp. 84-105, Elsevier BV [doi]  [abs]
127. Balajewicz, M; Tezaur, I; Dowell, E, Minimal subspace rotation on the Stiefel manifold for stabilization and enhancement of projection-based reduced order models for the compressible Navier-Stokes equations, Journal of Computational Physics, vol. 321 (September, 2016), pp. 224-241, Elsevier BV [doi]  [abs]
128. Lin, H; Wang, S; Dowell, EH; Dong, J; Ma, C, Dynamic characteristics of double-helical planetary gear sets under time-varying mesh stiffness, Journal of Harbin Institute of Technology (New Series), vol. 23 no. 4 (August, 2016), pp. 44-51 [doi]  [abs]
129. Chueshov, I; Dowell, EH; Lasiecka, I; Webster, JT, Nonlinear Elastic Plate in a Flow of Gas: Recent Results and Conjectures, Applied Mathematics & Optimization, vol. 73 no. 3 (June, 2016), pp. 475-500, Springer Nature [doi]  [abs]
130. Tang, D; Dowell, EH, Experimental aeroelastic models design and wind tunnel testing for correlation with new theory, Aerospace, vol. 3 no. 2 (June, 2016), pp. 12-12, MDPI AG [doi]  [abs]
131. Dowell, EH; McHugh, K, Equations of Motion for an Inextensible Beam or Plate Undergoing Large Deflections, Journal of Applied Mechanics, vol. 83 no. 5 (May, 2016), pp. 051007-051007, American Society of Mechanical Engineers (ASME), ISSN 1528-9036 [doi]  [abs]
132. Ganji, HF; Dowell, EH, Panel flutter prediction in two dimensional flow with enhanced piston theory, Journal of Fluids and Structures, vol. 63 (May, 2016), pp. 97-102, Elsevier BV [doi]  [abs]
133. Besem, FM; Thomas, JP; Kielb, RE; Dowell, EH, An aeroelastic model for vortex-induced vibrating cylinders subject to frequency lock-in, Journal of Fluids and Structures, vol. 61 (February, 2016), pp. 42-59, Elsevier BV [doi]  [abs]
134. Dowell, EH; Chueshov, I; Lasiecka, I; Webster, JT, Mathematical Aeroelasticity: A Survey, Journal of Dynamics and Differential Equations (January, 2016), ISSN 1572-9222
135. Dowell, EH; culver, D, High Frequency Response of a Nonlinear Spring-Mass System Attached to a Plate, Journal of Sound and Vibration (January, 2016), ISSN 1095-8568
136. Dowell, EH; Greenberg, J, Aerodynamic Modes in a Box, Aiaa Journal (January, 2016), American Institute of Aeronautics and Astronautics, ISSN 1533-385X
137. Dowell, EH, Far field predicted by piston theory, Aiaa Journal, vol. 54 no. 1 (January, 2016), pp. 364-366, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
138. Padmanabhan, MA; Dowell, EH; Thomas, JP; Pasiliao, CL, Store-induced limit-cycle oscillations due to nonlinear wing-store attachment, Journal of Aircraft, vol. 53 no. 3 (January, 2016), pp. 778-789, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
139. Bejan, A; Charles, JD; Lorente, S; Dowell, EH, Evolution of airplanes, and what price speed?, Aiaa Journal, vol. 54 no. 3 (January, 2016), pp. 1116-1119, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
140. Lin, H; Wang, S; Dowell, EH; Dong, J, Bifurcation Observation of Combining Spiral Gear Transmission Based on Parameter Domain Structure Analysis, Mathematical Problems in Engineering, vol. 2016 (January, 2016), pp. 1-13, Hindawi Limited [doi]  [abs]
141. Xie, D; Xu, M; Dai, H; Dowell, EH, Proper orthogonal decomposition method for analysis of nonlinear panel flutter with thermal effects in supersonic flow, Journal of Sound and Vibration, vol. 337 (February, 2015), pp. 263-283, Elsevier BV, ISSN 0022-460X [doi]  [abs]
142. Liu, L; Zhu, C; Yu, Z; Dowell, EH, Guidance and ignition control of lateral-jet-controlled interceptor missiles, Journal of Guidance, Control, and Dynamics, vol. 38 no. 12 (January, 2015), pp. 2455-2460, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0731-5090 [doi]  [abs]
143. Wilkie, WK; Warren, JE; Horta, LG; Lyle, KH; Juang, JN; Gibbs, SC; Dowell, EH; Guerrant, DV; Lawrence, D, Recent advances in heliogyro solar sail structural dynamics, stability, and control research, 2nd Aiaa Spacecraft Structures Conference (January, 2015), ISBN 9781624103452  [abs]
144. Dowell, EH, Stall flutter, Solid Mechanics and Its Applications, vol. 217 (January, 2015), pp. 265-284, Springer International Publishing, ISSN 0925-0042 [doi]  [abs]
145. Dowell, EH, Aeroelastic control, Solid Mechanics and Its Applications, vol. 217 (January, 2015), pp. 531-584, Springer International Publishing, ISSN 0925-0042 [doi]  [abs]
146. Padmanabhan, MA; Pasiliao, CL; Dowell, EH, Store-induced limit cycle oscillations due to nonlinear wing-store attachment, 56th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (January, 2015), ISBN 9781624103421  [abs]
147. Goldman, BD; Dowell, EH; Scott, RC, In-flight aeroelastic stability of the thermal protection system on the NASA HIAD, part II: Nonlinear theory and extended aerodynamics, 56th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (January, 2015), ISBN 9781624103421  [abs]
148. Padmanabhan, MA; Dowell, EH, Landing gear design/maintenance analysis for nonlinear shimmy, Journal of Aircraft, vol. 52 no. 5 (January, 2015), pp. 1707-1710, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
149. Mannarino, A; Dowell, EH, Reduced-order models for computational-fluid-dynamics-based nonlinear aeroelastic problems, Aiaa Journal, vol. 53 no. 9 (January, 2015), pp. 2671-2685, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
150. Dowell, EH; Bliss, DB, Erratum: New look at unsteady supersonic potential flow aerodynamics and piston theory (AIAA Journal (2013) 51:9 (2278-2281)), Aiaa Journal, vol. 53 no. 8 (January, 2015), pp. 2419, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0731-5090 [Gateway.cgi], [doi]
151. Tang, D; Gibbs, SC; Dowell, EH, Nonlinear aeroelastic analysis with inextensible plate theory including correlation with experiment, Aiaa Journal, vol. 53 no. 5 (January, 2015), pp. 1299-1308, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
152. Gibbs, SC; Wang, I; Dowell, EH, Stability of rectangular plates in subsonic flow with various boundary conditions, Journal of Aircraft, vol. 52 no. 2 (January, 2015), pp. 439-451, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
153. Goldman, BD; Dowell, EH; Scott, RC, Aeroelastic stability of thermal protection system for inflatable aerodynamic decelerator, Journal of Spacecraft and Rockets, vol. 52 no. 1 (January, 2015), pp. 144-156, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0022-4650 [doi]  [abs]
154. Wei, Y; Chen, Z; Dowell, EH, CFD analysis of aerodynamic coefficients in labyrinth brush seal, Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece), vol. 4A-2015 (January, 2015), ASME, ISBN 9780791857397 [doi]  [abs]
155. Thomas, JP; Dowell, EH, Discrete adjoint design optimization approach for increasing transonic buffet onset angle-of-attack, 16th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference (January, 2015), ISBN 9781624103681  [abs]
156. Wilkie, WK; Warren, JE; Horta, LG; Lyle, KH; Juang, JN; Gibbs, SC; Dowell, EH; Guerrant, DV; Lawrence, D, Recent advances in heliogyro solar sail structural dynamics, stability, and control research, 2nd Aiaa Spacecraft Structures Conference (January, 2015), ISBN 9781624103452 [doi]  [abs]
157. Padmanabhan, MA; Pasiliao, CL; Dowell, EH, Store-induced limit cycle oscillations due to nonlinear wing-store attachment, 56th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (January, 2015), ISBN 9781624103421 [doi]  [abs]
158. Thomas, JP; Dowell, EH, Discrete adjoint design optimization approach for increasing transonic buffet onset angle-of-attack, 16th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference (January, 2015), ISBN 9781624103681 [doi]  [abs]
159. Goldman, BD; Dowell, EH; Scott, RC, In-flight aeroelastic stability of the thermal protection system on the NASA HIAD, part II: Nonlinear theory and extended aerodynamics, 56th Aiaa/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (January, 2015), ISBN 9781624103421 [doi]  [abs]
160. Tang, D; Dowell, EH, Effects of a free-to-roll fuselage on wing flutter: Theory and experiment, Aiaa Journal, vol. 52 no. 12 (December, 2014), pp. 2625-2632, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
161. Gibbs, SC; Dowell, EH, Membrane paradox for solar sails, Aiaa Journal, vol. 52 no. 12 (December, 2014), pp. 2904-2906, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
162. Yan, S; Dowell, EH; Lin, B, Effects of nonlinear damping suspension on nonperiodic motions of a flexible rotor in journal bearings, Nonlinear Dynamics, vol. 78 no. 2 (October, 2014), pp. 1435-1450, ISSN 0924-090X [doi]  [abs]
163. Xie, D; Xu, M; Dai, H; Dowell, EH, Observation and evolution of chaos for a cantilever plate in supersonic flow, Journal of Fluids and Structures, vol. 50 (October, 2014), pp. 271-291, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
164. Padmanabhan, MA; Pasiliao, CL; Dowell, EH, Simulation of aeroelastic limit-cycle oscillations of aircraft wings with stores, Aiaa Journal, vol. 52 no. 10 (October, 2014), pp. 2291-2299, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
165. Goldman, BD; Dowell, EH, Nonlinear oscillations of a fluttering plate resting on a unidirectional elastic foundation, Aiaa Journal, vol. 52 no. 10 (October, 2014), pp. 2364-2368, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
166. Tang, D; Zhao, M; Dowell, EH, Inextensible beam and plate theory: Computational analysis and comparison with experiment, Journal of Applied Mechanics, vol. 81 no. 6 (June, 2014), pp. 061009-061009, ASME International, ISSN 0021-8936 [doi]  [abs]
167. Eugeni, M; Dowell, EH; Mastroddi, F, Post-buckling longterm dynamics of a forced nonlinear beam: A perturbation approach, Journal of Sound and Vibration, vol. 333 no. 9 (April, 2014), pp. 2617-2631, ISSN 0022-460X [doi]  [abs]
168. Wu, ZY; Dowell, EH; Tang, DM, Damping analysis in beams subject to presliding friction, Mechanics Based Design of Structures and Machines, vol. 42 no. 2 (April, 2014), pp. 229-243, Informa UK Limited, ISSN 1539-7734 [doi]  [abs]
169. Goldman, BD; Dowell, EH; Scott, RC, In-flight aeroelastic stability of the thermal protection system on the NASA HIAD, Part I: Linear theory, 55th Aiaa/Asme/Asce/Ahs/Sc Structures, Structural Dynamics, and Materials Conference (February, 2014), American Institute of Aeronautics and Astronautics [doi]  [abs]
170. Xie, D; Xu, M; Dowell, EH, Proper orthogonal decomposition reduced-order model for nonlinear aeroelastic oscillations, Aiaa Journal, vol. 52 no. 2 (February, 2014), pp. 229-241, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
171. Xie, D; Xu, M; Dowell, EH, Projection-free proper orthogonal decomposition method for a cantilever plate in supersonic flow, Journal of Sound and Vibration, vol. 333 no. 23 (January, 2014), pp. 6190-6208, ISSN 0022-460X [doi]  [abs]
172. Thomas, JP; Dowell, EH, Discrete adjoint approach for aeroelastic design optimization, Aiaa Aviation 2014 15th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference (January, 2014), ISBN 9781624102837  [abs]
173. Gibbs, SC; Warren, JE; Wilkie, WK; Dowell, EH, Stability of rotorcraft for interplanetary space flight, Annual Forum Proceedings Ahs International, vol. 1 (January, 2014), pp. 471-479, ISSN 1552-2938  [abs]
174. Gibbs, CC; Sethna, A; Wang, I; Tang, D; Dowell, E, Aeroelastic stability of a cantilevered plate in yawed subsonic flow, Journal of Fluids and Structures, vol. 49 (January, 2014), pp. 450-462, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
175. Tang, D; Dowell, EH, Experimental aerodynamic response for an oscillating airfoil in buffeting flow, Aiaa Journal, vol. 52 no. 6 (January, 2014), pp. 1170-1179, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
176. Gibbs, SC; Fichera, S; Zanotti, A; Ricci, S; Dowell, EH, Flow field around the flapping flag, Journal of Fluids and Structures, vol. 48 (January, 2014), pp. 507-513, ISSN 0889-9746 [doi]  [abs]
177. Eftekhari, SA; Bakhtiari-Nejad, F; Dowell, EH, Damage detection of an aeroelastic panel using limit cycle oscillation analysis, International Journal of Non Linear Mechanics, vol. 58 (January, 2014), pp. 99-110, Elsevier BV, ISSN 0020-7462 [doi]  [abs]
178. Gibbs, SC; Fichera, S; Zanotti, A; Ricci, S; Dowell, EH, Flow field around the flapping flag, Journal of Fluids and Structures, vol. 48 (2014), pp. 507-513, Elsevier BV, ISSN 0889-9746 [doi]
179. Eugeni, M; Dowell, EH; Mastroddi, F, Post-buckling longterm dynamics of a forced nonlinear beam: A perturbation approach, Journal of Sound and Vibration, vol. 333 no. 9 (2014), pp. 2617-2631, Elsevier BV, ISSN 0022-460X [doi]
180. Tang, D; Dowell, EH, Experimental aeroelastic response for a freeplay control surface in buffeting flow, Aiaa Journal, vol. 51 no. 12 (December, 2013), pp. 2852-2861, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
181. Dowell, EH; Bliss, DB, New look at unsteady supersonic potential flow aerodynamics and piston theory, Aiaa Journal, vol. 51 no. 9 (September, 2013), pp. 2278-2281, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [Gateway.cgi], [doi]  [abs]
182. Thomas, JP; Dowell, EH; Hall, KC, Discrete adjoint method for nonlinear aeroelastic sensitivities for compressible and viscous flows, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (August, 2013), ISSN 0273-4508, ISBN 9781624102233  [abs]
183. Padmanabhan, MA; Pasiliao, CL; Dowell, EH, An approach to aeroelastic modeling and simulation of limit cycle oscillations of aircraft wings with stores, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (August, 2013), ISSN 0273-4508  [abs]
184. Wang, I; Chad Gibbs, S; Dowell, EH, Aeroelastic analysis of a folding wing: Comparison of simple and higher fidelity models for a wide range of fold angles, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (August, 2013), ISSN 0273-4508  [abs]
185. Gibbs, SC; Guerrant, DV; Wilkie, WK; Dowell, EH, Rectangular solar sail flutter, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (August, 2013), ISSN 0273-4508  [abs]
186. Padmanabhan, MA; Pasiliao, CL; Dowell, EH, An approach to aeroelastic modeling and simulation of Limit Cycle Oscillations of aircraft wings with stores, 54th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (August, 2013) [doi]  [abs]
187. Thomas, JP; Dowell, EH; Hall, KC, Discrete adjoint method for nonlinear aeroelastic sensitivities for compressible and viscous flows, 54th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (August, 2013), American Institute of Aeronautics and Astronautics, ISBN 9781624102233 [doi]  [abs]
188. Gibbs, SC; Guerrant, DV; Wilkie, WK; Dowell, EH, Rectangular solar sail flutter, 54th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (August, 2013), American Institute of Aeronautics and Astronautics [doi]  [abs]
189. Wang, I; Chad Gibbs, S; Dowell, EH, Aeroelastic analysis of a folding wing: Comparison of simple and higher fidelity models for a wide range of fold angles, 54th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (August, 2013), American Institute of Aeronautics and Astronautics [doi]  [abs]
190. Goldman, BD; Dowell, EH; Scott, RC, Flutter analysis of the thermal protection layer on the NASA HIAD, Aiaa Aerodynamic Decelerator Systems (Ads) Conference 2013 (August, 2013), American Institute of Aeronautics and Astronautics [doi]  [abs]
191. Grasch, AD; Jaworski, JW; Tang, D; Dowell, EH, Resonant frequency determination of a multistore high-altitude/long- endurance wing, Aiaa Journal, vol. 51 no. 6 (June, 2013), pp. 1277-1283, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
192. Thomas, JP; Custer, CH; Dowell, EH; Hall, KC; Corre, C, Compact implementation strategy for a harmonic balance method within implicit flow solvers, Aiaa Journal, vol. 51 no. 6 (June, 2013), pp. 1374-1381, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
193. Nefske, DJ; Sung, SH; Dowell, EH, Comment on "On Dowell's simplification for acoustic cavity-structure interaction and consistent alternatives [J. Acoust. Soc. Am. 127, 22-32 (2010)]"., The Journal of the Acoustical Society of America, vol. 133 no. 3 (March, 2013), pp. 1222-1224, ISSN 0001-4966 [Gateway.cgi], [doi]  [abs]
194. Hall, KC; Ekici, K; Thomas, JP; Dowell, EH, Harmonic balance methods applied to computational fluid dynamics problems, International Journal of Computational Fluid Dynamics, vol. 27 no. 2 (February, 2013), pp. 52-67, ISSN 1061-8562 [Gateway.cgi], [doi]  [abs]
195. Tang, D; Dowell, EH, Computational/experimental aeroelastic study for a horizontal-tail model with free play, Aiaa Journal, vol. 51 no. 2 (February, 2013), pp. 341-352, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [Gateway.cgi], [doi]  [abs]
196. Shen, Y; Liu, L; Dowell, EH, Adaptive fault-tolerant robust control for a linear system with adaptive fault identification, Iet Control Theory & Applications, vol. 7 no. 2 (January, 2013), pp. 246-252, Institution of Engineering and Technology (IET), ISSN 1751-8644 [doi]  [abs]
197. Eugeni, M; Mastroddi, F; Dowell, EH, Nonlinear aeroelastic response of a flat panel. A normal form approach, Ifasd 2013 International Forum on Aeroelasticity and Structural Dynamics (January, 2013)  [abs]
198. Balajewicz, MJ; Dowell, EH; Noack, BR, Low-dimensional modelling of high-Reynolds-number shear flows incorporating constraints from the Navier-Stokes equation, Journal of Fluid Mechanics, vol. 729 (January, 2013), pp. 285-308, Cambridge University Press (CUP), ISSN 0022-1120 [doi]  [abs]
199. Wang, I; Gibbs IV, SC; Dowell, EH, Flutter of rectangular plates in three dimensional incompressible flow with various boundary conditions: Theory and experiment, Proceedings of the Asme Design Engineering Technical Conference, vol. 1 no. PARTS A AND B (December, 2012), pp. 51-63, ASME [doi]  [abs]
200. Gibbs, SC; Wang, I; Bloomhardt, E; Dowell, EH, Aeroelastic behavior of noise-reducing membranes for aircraft lifting surfaces part I: Theory, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2012)  [abs]
201. Raveh, DE; Dowell, EH, Aeroelastic responses of spring-suspended airfoil systems in transonic buffeting flows, 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012 (December, 2012)  [abs]
202. Wang, I; Gibbs, SC; Bloomhardt, EM; Dowell, EH, Aeroelastic behavior of noise-reducing membranes for aircraft lifting surfaces part II: Experimen, 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012 (December, 2012)  [abs]
203. Ni, K; Hu, P; Zhao, H; Dowell, EH, Flutter and lco of an all-movable horizontal tail with freeplay, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2012)  [abs]
204. Ni, K; Hu, P; Zhao, H; Dowell, EH, Flutter and LCO of an all-movable horizontal tail with freeplay, 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012 (December, 2012), ISSN 0273-4508  [abs]
205. Raveh, DE; Dowell, EH, Aeroelastic responses of spring-suspended airfoil systems in transonic buffeting flows, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2012), ISSN 0273-4508  [abs]
206. Gibbs, SC; Wang, I; Bloomhardt, E; Dowell, EH, Aeroelastic behavior of noise-reducing membranes for aircraft lifting surfaces part I: Theory, 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012 (December, 2012), ISSN 0273-4508  [abs]
207. Thomas, JP; Dowell, EH; Hall, KC, An automatic differentiation based nonlinear reduced order modeling technique for unsteady separated flows, 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (December, 2012), American Institute of Aeronautics and Astronautics [doi]  [abs]
208. Jaworski, JW; Dowell, EH, Scaling analysis for aeroelastic phenomena using the navier-stokes fluid model, Aiaa Journal, vol. 50 no. 11 (November, 2012), pp. 2622-2626, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
209. Chad Gibbs, S; Wang, I; Dowell, E, Theory and experiment for flutter of a rectangular plate with a fixed leading edge in three-dimensional axial flow, Journal of Fluids and Structures, vol. 34 (October, 2012), pp. 68-83, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
210. Balajewicz, M; Dowell, EH, Stabilization of projection-based reduced order models of the Navier-Stokes, Nonlinear Dynamics, vol. 70 no. 2 (October, 2012), pp. 1619-1632, Springer Nature, ISSN 0924-090X [doi]  [abs]
211. Liu, L; Shen, Y; Dowell, EH; Zhu, C, A general H ∞ fault tolerant control and management for a linear system with actuator faults, Automatica, vol. 48 no. 8 (August, 2012), pp. 1676-1682, Elsevier BV, ISSN 0005-1098 [doi]  [abs]
212. Balajewicz, M; Dowell, E, Reduced-order modeling of flutter and limit-cycle oscillations using the sparse volterra series, Journal of Aircraft, vol. 49 no. 6 (January, 2012), pp. 1803-1812, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
213. Eftekhari, SA; Bakhtiari-Nejad, F; Dowell, EH, An investigation on the sensitivity of limit cycle oscillations for detecting damage in an aeroelastic panel, Applied Mechanics and Materials, vol. 110-116 (January, 2012), pp. 4424-4432, Trans Tech Publications, ISSN 1660-9336 [doi]  [abs]
214. Stanton, SC; Erturk, A; Mann, BP; Dowell, EH; Inman, DJ, Nonlinear nonconservative behavior and modeling of piezoelectric energy harvesters including proof mass effects, Journal of Intelligent Material Systems and Structures, vol. 23 no. 2 (January, 2012), pp. 183-199, SAGE Publications, ISSN 1045-389X [doi]  [abs]
215. Liu, L; Shen, Y; Dowell, EH, Integrated adaptive fault-tolerant H∞ output feedback control with adaptive fault identification, Journal of Guidance, Control, and Dynamics, vol. 35 no. 3 (January, 2012), pp. 881-889, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0731-5090 [doi]  [abs]
216. Wang, I; Gibbs, SC; Dowell, EH, Aeroelastic model of multisegmented folding wings: Theory and experiment, Journal of Aircraft, vol. 49 no. 3 (January, 2012), pp. 911-921, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
217. Raveh, DE; Dowell, EH, Aeroelastic responses of spring-suspended airfoil systems in transonic buffeting flows, 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012 (January, 2012), ISBN 9781600869372 [doi]  [abs]
218. Ni, K; Hu, P; Zhao, H; Dowell, EH, Flutter and LCO of an all-movable horizontal tail with freeplay, 53rd Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference 2012 (January, 2012), ISBN 9781600869372 [doi]  [abs]
219. Thomas, JP; Dowell, EH, Airfoil transonic flow buffet calculations using the OVERFLOW 2 flow solver, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2011), American Institute of Aeronautics and Astronautics, ISSN 0273-4508 [doi]  [abs]
220. Bloomhardt, EM; Dowell, EH, A study of the aeroelastic behavior of flat plates and membranes with mixed boundary conditions in axial subsonic flow, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2011), American Institute of Aeronautics and Astronautics, ISSN 0273-4508 [repository], [doi]  [abs]
221. Dunnmon, JA; Stanton, SC; Mann, BP; Dowell, EH, Aeroelastic limit cycles as a small scale energy source, Proceedings of the Asme Design Engineering Technical Conference, vol. 4 no. PARTS A AND B (December, 2011), pp. 1181-1190 [doi]  [abs]
222. Wang, I; Dowell, EH, A structural dynamics model of a multi-segmented folding wing: Theory and experiment, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 48 no. 6 (December, 2011), pp. 2149-2160, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
223. Dunnmon, JA; Stanton, SC; Mann, BP; Dowell, EH, Power extraction from aeroelastic limit cycle oscillations, Journal of Fluids and Structures, vol. 27 no. 8 (November, 2011), pp. 1182-1198, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
224. Dowell, EH, Can solar sails flutter?, Aiaa Journal, vol. 49 no. 6 (June, 2011), pp. 1305-1306, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]
225. Eftekhari, SA; Bakhtiari-Nejad, F; Dowell, EH, Bifurcation boundary analysis as a nonlinear damage detection feature: Does it work?, Journal of Fluids and Structures, vol. 27 no. 2 (February, 2011), pp. 297-310, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
226. Wang, I; Dowell, EH, Structural Dynamics model of multisegmented folding wings: Theory and experiment, Journal of Aircraft, vol. 48 no. 6 (January, 2011), pp. 2149-2160, ISSN 0273-4508 [doi]  [abs]
227. Raveh, DE; Dowell, EH, Frequency lock-in phenomenon for oscillating airfoils in buffeting flows, Journal of Fluids and Structures, vol. 27 no. 1 (January, 2011), pp. 89-104, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
228. Liu, L; Shen, Y; Zhu, C; Dowell, EH, Online selection of H∞ controllers for a faulty linear system, Proceedings of the Ieee Conference on Decision and Control (January, 2011), pp. 2257-2262, IEEE, ISSN 0191-2216 [doi]  [abs]
229. Tang, D; Dowell, EH, Aeroelastic response induced by free play, Part 1: Theory, Aiaa Journal, vol. 49 no. 11 (January, 2011), pp. 2532-2542, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
230. Tang, D; Dowell, EH, Aeroelastic analysis and experiment for wing/store model with stiction nonlinearity, Journal of Aircraft, vol. 48 no. 5 (January, 2011), pp. 1512-1530, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
231. Tang, D; Dowell, EH, Aeroelastic response induced by free play, Part 2: Theoretical/experimental correlation analysis, Aiaa Journal, vol. 49 no. 11 (January, 2011), pp. 2543-2554, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
232. Dowell, EH, Some recent advances in nonlinear aeroelasticity: Fluid-structure interaction in the 21 ^st Century, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2010), ISSN 0273-4508  [abs]
233. Thomas, JP; Custer, CH; Dowell, EH; Hall, KC, F-16 fighter aeroelastic computations using a harmonic balance implementation of the OVERFLOW 2 flow solver, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2010), ISSN 0273-4508, ISBN 9781600867422  [abs]
234. Hu, P; Ni, K; Qu, K; Xue, L; Zhao, H; Dowell, EH, An efficient POD/ROM based aeroelasticity model, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (December, 2010), ISSN 0273-4508  [abs]
235. Tang, D; Grasch, A; Dowell, EH, Gust response for flexibly suspended high-aspect ratio wings, Aiaa Journal, vol. 48 no. 10 (October, 2010), pp. 2430-2444, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
236. Dowell, EH, Comment on "On Dowell's simplification for acoustic cavity-structure interaction and consistent alternatives" [J. Acoust. Soc. Am. 127, 22-32 (2010)]., The Journal of the Acoustical Society of America, vol. 128 no. 1 (July, 2010), pp. 1-2 [20649193], [doi]
237. Dowell, EH, Transonic unsteady potential flow: Scaling analysis of linear and nonlinear dynamics, Aiaa Journal, vol. 48 no. 5 (May, 2010), pp. 1017-1019, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
238. Tang, D; Dowell, EH, Aeroelastic airfoil with free play at angle of attack with gust excitation, Aiaa Journal, vol. 48 no. 2 (February, 2010), pp. 427-442, ISSN 0001-1452 [doi]  [abs]
239. Thomas, JP; Dowell, EH; Hall, KC, Using automatic differentiation to create a nonlinear reduced-order-model aerodynamic solver, Aiaa Journal, vol. 48 no. 1 (January, 2010), pp. 19-24, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
240. Lee, DH; Chen, PC; Tang, D; Dowell, EH, Nonlinear gust response of a control surface with free-play, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference (January, 2010), ISSN 0273-4508 [doi]  [abs]
241. Attar, PJ; Tang, D; Dowell, EH, Nonlinear aeroelastic study for folding wing structures, Aiaa Journal, vol. 48 no. 10 (January, 2010), pp. 2187-2195, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
242. Hu, P; Qu, K; Xue, L; Ni, K; Dowell, E, Efficient aeroelastic model updating in support of flight testing, Aiaa Atmospheric Flight Mechanics Conference (December, 2009)  [abs]
243. Liu, L; Dowell, EH, High dimensional harmonic balance analysis for dynamic piecewise aeroelastic systerms, Asme International Mechanical Engineering Congress and Exposition, Proceedings, vol. 12 (September, 2009), pp. 659-669  [abs]
244. Liska, S; Dowell, EH, Continuum aeroelastic model for a folding-wing configuration, Aiaa Journal, vol. 47 no. 10 (January, 2009), pp. 2350-2358, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [Gateway.cgi], [doi]  [abs]
245. Thomas, JP; Custer, CH; Dowell, EH; Hall, KC, Unsteady flow computation using a harmonic balance approach implemented about the OVERFLOW 2 flow solver, 19th Aiaa Computational Fluid Dynamics Conference (January, 2009), ISBN 9781563479755 [doi]  [abs]
246. Dowell, EH; Thomas, JP; Hall, KC; Denegri, CM, Theoretical predictions of F-16 fighter limit cycle oscillations for flight flutter testing, Journal of Aircraft, vol. 46 no. 5 (January, 2009), pp. 1667-1672, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
247. Schwarz, JB; Dowell, EH; Thomas, JP; Hall, KC; Rausch, RD; Bartels, RE, Improved flutter boundary prediction for an isolated two-degree-of-freedom airfoil, Journal of Aircraft, vol. 46 no. 6 (January, 2009), pp. 2069-2076, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
248. Jaworski, JW; Dowell, EH, Comparison of theoretical structural models with experiment for a high-aspect-ratio aeroelastic wing, Journal of Aircraft, vol. 46 no. 2 (January, 2009), pp. 708-713, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
249. Tang, D; Dowell, EH, Flutter/LCO suppression for high-aspect ratio wings, The Aeronautical Journal, vol. 113 no. 1144 (January, 2009), pp. 409-416, Cambridge University Press (CUP), ISSN 0001-9240 [doi]  [abs]
250. Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Li, A; Denegri, CM, Reduced order models in unsteady aerodynamic models, aeroelasticity and molecular dynamics, Icas Secretariat 26th Congress of International Council of the Aeronautical Sciences 2008, Icas 2008, vol. 1 (December, 2008), pp. 4002-4014, ISBN 9781605607153  [abs]
251. Liu, L; Kalmár-Nagy, T; Dowell, EH, The high dimensional harmonic balance analysis for second-order delay-differential equations, 2007 Proceedings of the Asme International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, Detc2007, vol. 5 PART A (June, 2008), pp. 695-702, ASME [doi]  [abs]
252. Ekici, K; Hall, KC; Dowell, EH, Computationally Fast Harmonic Balance Methods for Unsteady Aerodynamic Predictions of Helicopter Rotors, Journal of Computational Physics, vol. 227 no. 12 (June, 2008), pp. 6206-6225, Elsevier, ISSN 0021-9991 [doi]  [abs]
253. Ekici, K; Hall, KC; Dowell, EH, Computationally fast harmonic balance methods for unsteady aerodynamic predictions of helicopter rotors, Journal of Computational Physics, vol. 227 no. 12 (June, 2008), pp. 6206-6225, Elsevier BV [doi]  [abs]
254. Jaworski, JW; Dowell, EH, Free vibration of a cantilevered beam with multiple steps: Comparison of several theoretical methods with experiment, Journal of Sound and Vibration, vol. 312 no. 4-5 (May, 2008), pp. 713-725, Elsevier BV, ISSN 0022-460X [doi]  [abs]
255. Virgin, LN; Dowell, EH; Flowers, G, Nonlinear Vibration (April, 2008), pp. 255-267, JOHN WILEY & SONS INC [doi]
256. Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Denegri, CM, A new solution method for unsteady flows around oscillating bluff bodies, IUTAM Bookseries, vol. 8 (January, 2008), pp. 37-44, Springer Netherlands, ISSN 1875-3507 [doi]
257. Attar, PJ; Dowell, EH; Tang, D, Delta wing with store limit-cycle-oscillation modeling using a high-fidelity structural model, Journal of Aircraft, vol. 45 no. 3 (January, 2008), pp. 1054-1061, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
258. Tang, D; Dowell, EH, Theoretical and experimental aeroelastic study for folding wing structures, Journal of Aircraft, vol. 45 no. 4 (January, 2008), pp. 1136-1147, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
259. Dowell, EH, Free vibrations of an arbitrary structure in terms of component modes, Trans. Asme, E, J. Appl. Mech. (Usa), vol. 39 no. 3 (2008), pp. 727-732  [abs]
260. Dowell, EH, Free vibrations of a linear structure with arbitrary support conditions, Trans. Asme, E, J. Appl. Mech. (Usa), vol. 38 no. 3 (2008), pp. 595-600  [abs]
261. Jaworski, JW; Dowell, EH, Supersonic indicial lift functions from transform methods, Aiaa Journal, vol. 45 no. 8 (August, 2007), pp. 2106-2111, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
262. Liu, L; Dowell, EH; Thomas, JP, A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces, Journal of Fluids and Structures, vol. 23 no. 3 (April, 2007), pp. 351-363, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
263. Tang, D; Dowell, EH, Aerodynamic loading for an airfoil with an oscillating gurney flap, Journal of Aircraft, vol. 44 no. 4 (January, 2007), pp. 1245-1257, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
264. Liu, LP; Dowell, EH; Hall, KC, A novel harmonic balance analysis for the Van Der Pol oscillator, International Journal of Non Linear Mechanics, vol. 42 no. 1 (January, 2007), pp. 2-12, Elsevier BV, ISSN 0020-7462 [doi]  [abs]
265. Dowell, EH, Non-linear theory of unstable plane Poiseuille flow, J. Fluid Mech. (Uk), vol. 38 no. 2 (2007), pp. 401-414, Cambridge University Press (CUP) [doi]  [abs]
266. Thomas, JP; Dowell, EH; Hall, KC; Denegri, CM, An investigation of the sensitivity of F-16 fighter flutter onset and limit cycle oscillations to uncertainties, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 5 (December, 2006), pp. 3137-3144, ISSN 0273-4508, ISBN 1563478080  [abs]
267. Tang, D; Dowell, EH, Experimental and theoretical study of gust response for a wing-store model with freeplay, Journal of Sound and Vibration, vol. 295 no. 3-5 (August, 2006), pp. 659-684, Elsevier BV, ISSN 0022-460X [doi]  [abs]
268. P. J. Attar and E. H. Dowell and J. R. White and J. P. Thomas, Reduced order nonlinear system identification methodology, Aiaa Journal, vol. 44 no. 8 (August, 2006), pp. 1895 -- 1904, ISSN 0001-1452  [abs]
269. D. Tang and P. Attar and A. Q. Li and E. H. Dowell, Complex dynamics of a pyranose ring structure molecule attached to an atomic force microscope, Nonlinear Dynamics, vol. 45 no. 3-4 (August, 2006), pp. 283 -- 303, ISSN 0924-090X  [abs]
270. Tang, D; Attar, P; Li, A; Dowell, EH, Complex dynamics of a pyranose ring structure molecule attached to an atomic force microscope, Nonlinear Dynamics, vol. 45 no. 3-4 (August, 2006), pp. 283-303, Springer Nature, ISSN 0924-090X [s11071-006-0508-9], [doi]  [abs]
271. Attar, PJ; Dowell, EH; White, JR; Thomas, JP, Reduced order nonlinear system identification methodology, Aiaa Journal, vol. 44 no. 8 (August, 2006), pp. 1895-1904, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [1.16221], [doi]  [abs]
272. D. Tang and P. Attar and E. H. Dowell, Flutter/limit cycle oscillation analysis and experiment for wing-store model, Aiaa Journal, vol. 44 no. 7 (July, 2006), pp. 1662 -- 1675, ISSN 0001-1452  [abs]
273. Tang, D; Attar, P; Dowell, EH, Flutter/limit cycle oscillation analysis and experiment for wing-store model, Aiaa Journal, vol. 44 no. 7 (July, 2006), pp. 1662-1675, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
274. L. Liu and J. P. Thomas and E. H. Dowell and P. Attar and K. C. Hall, A comparison of classical and high dimensional harmonic balance approaches for a Duffing oscillator, Journal Of Computational Physics, vol. 215 no. 1 (June, 2006), pp. 298 -- 320, ISSN 0021-9991  [abs]
275. Thomas, JP; Dowell, EH; Hall, KC, Using automatic differentiation to create a nonlinear reduced order model of a computational fluid dynamic solver, Collection of Technical Papers 11th Aiaa/Issmo Multidisciplinary Analysis and Optimization Conference, vol. 4 (January, 2006), pp. 2437-2449, Portsmouth, VA, United States, ISBN 1563478234 [doi]  [abs]
276. Spiker, MA; Thomas, JP; Hall, KC; Kielb, RE; Dowell, EH, Modeling cylinder flow vortex shedding with enforced motion using a harmonic balance approach, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 7 (January, 2006), pp. 4549-4558, ISSN 0273-4508, ISBN 1563478080 [doi]  [abs]
277. Tang, D; Dowell, EH, Aerodynamic flow control of an airfoil with small trailing-edge strips, Journal of Aircraft, vol. 43 no. 6 (January, 2006), pp. 1854-1866, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
278. Attar, PJ; Dowell, EH, Stochastic analysis of a nonlinear aeroelastic model using the response surface method, Journal of Aircraft, vol. 43 no. 4 (January, 2006), pp. 1044-1052, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [1.17525], [doi]  [abs]
279. Attar, PJ; Dowell, EH, Erratum: Stochastic analysis of a nonlinear aeroelastic model using the response surface method (Journal of Aircraft (2006) (1044)), Journal of Aircraft, vol. 43 no. 6 (January, 2006), pp. 1959, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [1.28838], [doi]
280. Li, A; Dowell, EH, Modal reduction of mathematical models of biological molecules, Journal of Computational Physics, vol. 211 no. 1 (January, 2006), pp. 262-288, Elsevier BV [021], [doi]  [abs]
281. Tang, D; Dowell, EH, Flutter and limit-cycle oscillations for a wing-store model with freeplay, Journal of Aircraft, vol. 43 no. 2 (January, 2006), pp. 487-503, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
282. Tang, D. and Dowell, E.H., Aerodynamic flow control of an airfoil with small trailing-edge strips, J. Aircr. (USA), vol. 43 no. 6 (2006), pp. 1854 - 66 [1.18969]  [abs]
283. Dowell, E.H. and Deman Tang, Experimental and theoretical study of gust response for a wing-store model with freeplay, J. Sound Vib. (UK), vol. 295 no. 3-5 (2006), pp. 659 - 84 [024]  [abs]
284. Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Denegri, CM, Reduced Order Models in Unsteady Aerodynamic Models, Aeroelasticity and Molecular Dynamics, vol. 6 (2006), pp. 247-267, Springer Netherlands, ISBN 9781402049781 [Gateway.cgi], [doi]
285. Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C, Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, Journal of Aircraft, vol. 43 no. 4 (2006), pp. 865-878, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
286. Liu, L; Thomas, JP; Dowell, EH; Attar, P; Hall, KC, A comparison of classical and high dimensional harmonic balance approaches for a Duffing oscillator, J. Comput. Phys. (Usa), vol. 215 no. 1 (2006), pp. 298-320, Elsevier BV, ISSN 0021-9991 [026], [doi]  [abs]
287. D. M. Tang and E. H. Dowell, Flutter and limit-cycle oscillations for a wing-store model with freeplay, Journal Of Aircraft, vol. 43 no. 2 (2006), pp. 487 -- 503, ISSN 0021-8669  [abs]
288. J. P. Thomas and E. H. Dowell and K. C. Hall, Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, Journal Of Aircraft, vol. 43 no. 4 (2006), pp. 865 -- 878, ISSN 0021-8669  [abs]
289. P. J. Attar and E. H. Dowell, Stochastic analysis of a nonlinear aeroelastic model using the response surface method, Journal Of Aircraft, vol. 43 no. 4 (2006), pp. 1044 -- 1052, ISSN 0021-8669  [abs]
290. Thomas, JP; Dowell, EH; Hall, KC; Denegri, CM, Further investigation of modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (December, 2005), pp. 1457-1466, Austin, TX, United States, ISSN 0273-4508  [abs]
291. Dowell, EH; Clark, R; Cox, D; Curtiss, HC; Edwards, JW; Hall, KC; Peters, DA; Scanlan, R; Simiu, E; Sisto, F; Strganac, TW, A modern course in aeroelasticity, vol. 116 (December, 2005), pp. 1-766, ISSN 0925-0042, ISBN 9781402020391
292. Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Denegri, CM, Reduced order unsteady aerodynamic models and aeroelasticity, 12th International Congress on Sound and Vibration 2005, Icsv 2005, vol. 1 (December, 2005), pp. 47-64, ISBN 9781627481496  [abs]
293. Tang, D; Attar, PJ; Dowell, EH, Experimental/theoretical correlation study of nonlinear aeroelasticity for a wing-store model with freeplay, 3rd M.I.T. Conference on Computational Fluid and Solid Mechanics (December, 2005), pp. 1187-1190  [abs]
294. Amabili, M; Dowell, E; Epureanu, BI, Special issue in honour of Professor Michael P. Païdoussis, Journal of Fluids and Structures, vol. 21 no. 5-7 SPEC. ISS. (December, 2005), pp. 441-447, Elsevier BV, ISSN 0889-9746 [doi]
295. Attar, PJ; Dowell, EH, A reduced order system ID approach to the modelling of nonlinear structural behavior in aeroelasticity, Journal of Fluids and Structures, vol. 21 no. 5-7 SPEC. ISS. (December, 2005), pp. 531-542, Elsevier BV, ISSN 0889-9746 [012], [doi]  [abs]
296. Xie, J; Ding, W; Dowell, EH; Virgin, LN, Hopf-flip bifurcation of high dimensional maps and application to vibro-impact systems, Acta Mechanica Sinica, vol. 21 no. 4 (August, 2005), pp. 402-410, Springer Nature, ISSN 0567-7718 [s10409-005-0045-7], [doi]  [abs]
297. Attar, PJ; Dowell, EH; Tang, D, Modeling the LCO of a delta wing with an external store using a high fidelity structural model, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 2 (January, 2005), pp. 1394-1411, Austin, TX, United States, ISSN 0273-4508 [doi]  [abs]
298. Liu, L; Dowell, EH; Thomas, JP, Higher order harmonic balance analysis for limit cycle oscillations in an airfoil with cubic restoring forces, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (January, 2005), pp. 1467-1476, Austin, TX, United States, ISSN 0273-4508 [doi]  [abs]
299. Attar, PJ; Dowell, EH, A stochastic analysis of the limit cycle behavior of a nonlinear aeroelastic model using the response surface method, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 4 (January, 2005), pp. 2318-2338, Austin, TX, United States, ISSN 0273-4508 [doi]  [abs]
300. Li, A; Dowell, EH, Modal reduction of mathematical models of biological molecules, Proceedings of the Asme International Design Engineering Technical Conferences and Computers and Information in Engineering Conference Detc2005, vol. 1 C (January, 2005), pp. 1801-1815, Long Beach, CA, United States [doi]  [abs]
301. Carlson, HA; Feng, JQ; Thomas, JP; Kielb, RE; Hall, KC; Dowell, EH, Computational models for nonlinear aeroelasticity, 43rd Aiaa Aerospace Sciences Meeting and Exhibit Meeting Papers (January, 2005), pp. 4143-4152, Reno, NV, United States [doi]  [abs]
302. Liu, L; Dowell, EH, Harmonic balance approach for an airfoil with a freeplay control surface, Aiaa Journal, vol. 43 no. 4 (January, 2005), pp. 802-815, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
303. Kanda, A; Dowell, EH, Worst-case gust-response analysis for typical airfoil section with control surface, Journal of Aircraft, vol. 42 no. 4 (January, 2005), pp. 956-962, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
304. Epureanu, BI; Yin, SH; Dowell, EH, Enhanced nonlinear dynamics for accurate identification of stiffness loss in a thermo-shielding panel, Nonlinear Dynamics, vol. 39 no. 1-2 (January, 2005), pp. 197-211, Springer Nature [s11071-005-1926-9], [doi]  [abs]
305. Attar, PJ; Dowell, EH; White, JR, Modeling delta wing limit-cycle oscillations using a high-fidelity structural model, Journal of Aircraft, vol. 42 no. 5 (January, 2005), pp. 1209-1217, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
306. Attar, PJ; Dowell, EM, A reduced order system ID approach to the modeling of nonlinear structural behavior in aeroelasticity, Proceedings of the Asme International Design Engineering Technical Conferences and Computers and Information in Engineering Conference Detc2005, vol. 1 B (January, 2005), pp. 1271-1279 [doi]  [abs]
307. Thomas Jeffrey, P; Hall Kenneth, C; Dowell Earl, H, Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities, Aiaa Journal, vol. 43 no. 9 (2005), pp. 1931-1936, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
308. Dowell Earl, H; Epureanu Bogdan, I, Nonlinear: Introduction, Nonlinear Dynamics, vol. 39 no. 1-2 (2005), pp. 1, Oxford University Press [s11071-005-6551-0], [doi]
309. Tang, D; Li, A; Attar, P; Dowell, EH, Reduced order dynamic model for polysaccharides molecule attached to an atomic force microscope, Journal of Computational Physics, vol. 201 no. 2 (December, 2004), pp. 723-752, Elsevier BV [016], [doi]  [abs]
310. Thomas, JP; Dowell, EH; Hall, KC; Denegri, CM, Modeling limit cycle oscillation behavior of the F-16 fighter using a harmonic balance approach, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (December, 2004), pp. 2044-2050, Palm Springs, CA, United States, ISSN 0273-4508  [abs]
311. Dowell, EH; Tang, DM, Nonlinear dynamics of very high dimensional fluid-structural systems, Fluid Mechanics and its Applications, vol. 75 (December, 2004), pp. 73-113, Springer Netherlands, ISSN 0926-5112 [doi]  [abs]
312. Tang, D; Dowell, EH, Dynamic analysis of a protein-ligand molecular chain attached to an atomic force microscope, Journal of Vibration and Acoustics, vol. 126 no. 4 (October, 2004), pp. 496-513, ASME International, ISSN 1048-9002 [1.1804999], [doi]  [abs]
313. Li, A; Dowell, EH, Asymptotic modal analysis of dynamical systems: The effect of modal cross-correlation, Journal of Sound and Vibration, vol. 276 no. 1-2 (September, 2004), pp. 65-80, Elsevier BV [031], [doi]  [abs]
314. Tang, D; Dowell, EH, Reduced order model analysis for two-dimensipnal molecular dynamic chain structure attached to an atomic force microscope, Journal of Dynamic Systems, Measurement, and Control, vol. 126 no. 3 (September, 2004), pp. 531-546, ASME International, ISSN 0022-0434 [doi]  [abs]
315. Liu, L; Dowell, EH, The secondary bifurcation of an aeroelastic airfoil motion: Effect of high harmonics, Nonlinear Dynamics, vol. 37 no. 1 (July, 2004), pp. 31-49, Springer Nature, ISSN 0924-090X [4d], [doi]  [abs]
316. Tang, D; Li, A; Dowell, EH, Transient response study on rolling effectiveness of multiple control surfaces, Journal of Fluids and Structures, vol. 19 no. 5 (June, 2004), pp. 621-634, Elsevier BV [006], [doi]  [abs]
317. Tang, D; Gavin, HP; Dowell, EH, Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 2: Experiment, Journal of Sound and Vibration, vol. 269 no. 3-5 (January, 2004), pp. 875-897, Elsevier BV [S0022-460X(03)00181-0], [doi]  [abs]
318. Tang, D; Gavin, HP; Dowell, EH, Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 1: Theory, Journal of Sound and Vibration, vol. 269 no. 3-5 (January, 2004), pp. 853-874, Elsevier BV [S0022-460X(03)00180-9], [doi]  [abs]
319. Attar, PJ; Dowell, EH; White, JR, Modeling the LCO of a delta wing using a high fidelity structural model, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (January, 2004), pp. 1986-2000, Palm Springs, CA, United States, ISSN 0273-4508 [doi]  [abs]
320. Tang, DM; Dowell, EH, Effects of geometric structural nonlinearity of flutter and limit cycle oscillations of high-aspect-ratio wings, Journal of Fluids and Structures, vol. 19 no. 3 (January, 2004), pp. 291-306, Elsevier BV [007], [doi]  [abs]
321. Dowell, E.H. and Thomas, J.P. and Hall, K.C., Transonic limit cycle oscillation analysis using reduced order aerodynamic models, Journal of Fluids and Structures, vol. 18 no. SUPPL (2004), pp. 17 - 27 [018]  [abs]
322. Kholodar Denis, B; Dowell Earl, H; Thomas Jeffrey, P; Hall Kenneth, C, Improved understanding of transonic flutter: A three-parameter flutter surface, Journal of Aircraft, vol. 41 no. 4 (2004), pp. 911-917, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
323. Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C, Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach, Journal of Aircraft, vol. 41 no. 6 (2004), pp. 1266-1274, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
324. Dowell, EH; Thomas, JP; Hall, KC, Transonic limit cycle oscillation analysis using reduced order aerodynamic models, Journal of Fluids and Structures, vol. 18 no. SUPPL (2004), pp. 17-27, Elsevier BV [018], [doi]  [abs]
325. Kholodar Denis, B; Dowell Earl, H; Thomas Jeffrey, P; Hall Kenneth, C, Limit-cycle oscillations of a typical airfoil in transonic flow, Journal of Aircraft, vol. 41 no. 5 (2004), pp. 1067-1072, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
326. Tang, D; Gavin, HP; Dowell, EH, Gust alleviation using an electro-magnetic dry friction damper, 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (December, 2003)  [abs]
327. Thomas, JP; Hall, KC; Dowell, EH, A discrete adjoint approach for modeling unsteady aerodynamic design sensitivities, 41st Aerospace Sciences Meeting and Exhibit (December, 2003), ISBN 9781624100994  [abs]
328. Dowell, E; Edwards, J; Strganac, TW, Nonlinear aeroelasticity, 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference, vol. 50 no. pt 2 (December, 2003), pp. 760-799, Tainan, Taiwan  [abs]
329. Thomas, JP; Hall, KC; Dowell, EH, A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow, 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (December, 2003), ISBN 9781624101007  [abs]
330. Thomas, JP; Dowell, EH; Hall, KC, Modeling limit cycle oscillations for an NLR 7301 airfoil aeroelastic configuration including correlation with experiment, 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (December, 2003), ISBN 9781624101007  [abs]
331. Thomas, JP; Hall, KC; Dowell, EH, A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 7 (August, 2003), pp. 4779-4784, Norfolk, VA, United States, ISBN 9781624101007  [abs]
332. Dowell, EH; Tang, D, Multiscale, multiphenomena modeling and simulation at the nanoscale: On constructing reduced-order models for nonlinear dynamical systems with many degrees-of-freedom, Journal of Applied Mechanics, vol. 70 no. 3 (May, 2003), pp. 328-338, ASME International [1.1558079], [doi]  [abs]
333. Attar, PJ; Dowell, EH; Tang, DM, A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model, Journal of Fluids and Structures, vol. 17 no. 2 (February, 2003), pp. 243-259, Elsevier BV [S0889-9746(02)00123-8], [doi]  [abs]
334. Tang, DM; Yamamoto, H; Dowell, EH, Flutter and limit cycle oscillations of two-dimensional panels in three-dimensional axial flow, Journal of Fluids and Structures, vol. 17 no. 2 (February, 2003), pp. 225-242, Elsevier BV [S0889-9746(02)00121-4], [doi]  [abs]
335. Attar, PJ; Dowell, EH; Tang, D, Modeling aerodynamic nonlinearities for two aeroelastic configurations: Delta wing and flapping flag, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 2003), pp. 12-22, Norfolk, VA, United States [doi]  [abs]
336. Dowell, E; Edwards, J; Strganac, TW, Nonlinear aeroelasticity, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 5 (January, 2003), pp. 3824-3847 [doi]  [abs]
337. Thomas, JP; Dowell, EH; Hall, KC, Modeling limit cycle oscillations for an NLR 7301 airfoil aeroelastic configuration including correlation with experiment, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 2003), pp. 289-297, Norfolk, VA, United States, ISBN 9781624101007 [doi]  [abs]
338. Tang, D; Gavin, HP; Dowell, EH, Theoretical/experimental study of gust alleviation using an electro-magnetic dry friction damper, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 2 (January, 2003), pp. 1092-1108, Norfolk, VA, United States [doi]  [abs]
339. Dowell, E; Edwards, J; Strganac, T, Nonlinear aeroelasticity, Journal of Aircraft, vol. 40 no. 5 (January, 2003), pp. 857-874, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
340. Tang, D; Li, A; Dowell, EH, Experimental and theoretical study on rolling effectiveness of multiple control surfaces, Aiaa Journal, vol. 41 no. 2 (January, 2003), pp. 160-167, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
341. Dowell, EH; Bliss, DB; Clark, RL, Aeroelastic wing with leading- and trailing-edge control surfaces, Journal of Aircraft, vol. 40 no. 3 (January, 2003), pp. 559-565, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
342. Tang, D; Dowell, EH, Reduced Order Model Analysis For Two Dimensional Molecular Dynamic Chain Structure Attached To An Atomic Force Microscope, American Society of Mechanical Engineers, Design Engineering Division (Publication) De, vol. 116 no. 2 (January, 2003), pp. 905-924, ASME, Washington, DC, United States, ISSN 1521-4613 [doi]  [abs]
343. Epureanu, BI; Dowell, EH, Localized basis function method for computing limit cycle oscillations, Nonlinear Dynamics, vol. 31 no. 2 (January, 2003), pp. 151-166 [A:1022081101766], [doi]  [abs]
344. Epureanu, BI; Dowell, EH, Compact methodology for computing limit-cycle oscillations in aeroelasticity, Journal of Aircraft, vol. 40 no. 5 (January, 2003), pp. 955-963, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
345. Dowell, E; Edwards, J; Strganac, TW, Nonlinear aeroelasticity, 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (January, 2003), ISBN 9781624101007 [doi]  [abs]
346. Thomas, JP; Hall, KC; Dowell, EH, A harmonic balance approach for modeling nonlinear aeroelastic behavior of wings in transonic viscous flow, 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference (January, 2003), ISBN 9781624101007 [doi]  [abs]
347. Thomas, JP; Hall, KC; Dowell, EH, A discrete adjoint approach for modeling unsteady aerodynamic design sensitivities, 41st Aerospace Sciences Meeting and Exhibit (January, 2003), ISBN 9781624100994 [doi]  [abs]
348. Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C, Three-dimensional transonic aeroelasticity using proper orthogonal decomposition-based reduced-order models, Journal of Aircraft, vol. 40 no. 3 (2003), pp. 544-551, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
349. Kholodar Denis, B; Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C, Parametric study of flutter for an airfoil in inviscid transonic flow, Journal of Aircraft, vol. 40 no. 2 (2003), pp. 303-313, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
350. Wilson, TL; Dowell, E, Today's ephemera, tomorrow's historical documentation: access options for artists files, J. Libr. Adm. (Usa), vol. 39 no. 2-3 (2003), pp. 43-60, Informa UK Limited [J111v39n02_05], [doi]  [abs]
351. Dowell, EH; Tang, D, Nonlinear aeroelasticity and unsteady aerodynamics, 40th Aiaa Aerospace Sciences Meeting and Exhibit (December, 2002)  [abs]
352. Tang, D; Dowell, EH, Limit cycle oscillations of two-dimensional panels in low subsonic flow, International Journal of Non Linear Mechanics, vol. 37 no. 7 (October, 2002), pp. 1199-1209, Elsevier BV, ISSN 0020-7462 [S0020-7462(01)00140-8], [doi]  [abs]
353. Trickley, ST; Virgin, LN; Dowell, EH, The stability of limit-cycle oscillations in a nonlinear aeroelastic system, Proceedings. Mathematical, Physical, and Engineering Sciences, vol. 458 no. 2025 (September, 2002), pp. 2203-2226, The Royal Society, ISSN 1364-5021 [0965], [doi]  [abs]
354. Kholodar, DB; Thomas, JP; Dowell, EH; Hall, KC, A parameter study of transonic airfoil flutter and limit cycle oscillation behavior, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 2002), pp. 64-79, Denver, CO  [abs]
355. Thomas, JP; Dowell, EH; Hall, KC, Modeling viscous transonic limit cycle oscillation behavior using a harmonic balance approach, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (January, 2002), pp. 1658-1666, Denver, CO [doi]  [abs]
356. Tang, DM; Henry, JK; Dowell, EH, Effects of steady angle of attack on nonlinear gust response of a delta wing model, Journal of Fluids and Structures, vol. 16 no. 8 (January, 2002), pp. 1093-1110, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
357. Tang, D; Dowell, EH, Experimental and theoretical study of gust response for high-aspect-ratio wing, Aiaa Journal, vol. 40 no. 3 (January, 2002), pp. 419-429, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
358. Juang, JN; Kholodar, D; Dowell, EH, System identification of a vortex lattice aerodynamic model, Aiaa Journal, vol. 40 no. 6 (January, 2002), pp. 1187-1196, American Institute of Aeronautics and Astronautics (AIAA), Reno, NV, USA [doi]  [abs]
359. Tang, D; Dowell, EH, Limit-cycle hysteresis response for a high-aspect-ratio wing model, Journal of Aircraft, vol. 39 no. 5 (January, 2002), pp. 885-888, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
360. Reichert, WM; Daniels-Race, T; Dowell, EH, Time-tested survival skills for a publish or perish environment, Journal of Engineering Education, vol. 91 no. 1 (January, 2002), pp. 133-137, WILEY, ISSN 1069-4730 [doi]  [abs]
361. Dowell, EH; Tang, D, Nonlinear aeroelasticity and unsteady aerodynamics, Aiaa Journal, vol. 40 no. 9 (January, 2002), pp. 1697-1707, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
362. Tang, D; Li, A; Dowell, EH, Transient response study on rolling effectiveness of multiple control surfaces, Asme International Mechanical Engineering Congress and Exposition, Proceedings, vol. 253 no. 1 (January, 2002), pp. 89-100 [doi]  [abs]
363. Thomas, JP; Dowell, EH; Hall, KC, A harmonic balance approach for modeling three-dimensional nonlinear unsteady aerodynamics and aeroelasticity, Asme International Mechanical Engineering Congress and Exposition, Proceedings, vol. 253 no. 2 (January, 2002), pp. 1323-1334, ISBN 0791836592 [doi]  [abs]
364. Thomas Jeffrey, P; Dowell Earl, H; Hall Kenneth, C, Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations, Aiaa Journal, vol. 40 no. 4 (2002), pp. 638-646, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
365. Epureanu, BI; Dowell, EH; Hall, KC, Mach number influence on reduced-order models of inviscid potential flows in turbomachinery, Trans. Asme, J. Fluids Eng. (Usa), vol. 124 no. 4 (2002), pp. 977-987, ASME International, ISSN 0098-2202 [1.1511165], [doi]  [abs]
366. Thomas, JP; Dowell, EH; Hall, KC, A static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, 39th Aerospace Sciences Meeting and Exhibit (December, 2001)  [abs]
367. Heeg, J; Dowell, EH, Characterizing aeroelastic systems using eigenanalysis, explicitly retaining the aerodynamic degrees of freedom, 19th Aiaa Applied Aerodynamics Conference (December, 2001)  [abs]
368. Dowell, EH; Tang, D, Mathematical model of a nanopaddle oscillator, Journal of Applied Physics, vol. 90 no. 11 (December, 2001), pp. 5606-5611, AIP Publishing [1.1415535], [doi]  [abs]
369. Dowell, EH; Thomas, JP; Hall, KC, Transonic limit cycle oscillation analysis using reduced order aerodynamic models, 19th Aiaa Applied Aerodynamics Conference (December, 2001)  [abs]
370. Thomas, JP; Dowell, EH; Hall, KC, Three-Dimensional transonic Aeroelasticity using proper orthogonal decomposition based reduced order models, 19th Aiaa Applied Aerodynamics Conference (December, 2001)  [abs]
371. Thomas, JP; Dowell, EH; Hall, KC, Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations, 19th Aiaa Applied Aerodynamics Conference (December, 2001)  [abs]
372. Epureanu, BI; Dowell, EH; Hall, KC, A parametric analysis of reduced order models of potential flows in turbomachinery using proper orthogonal decomposition, Proceedings of the Asme Turbo Expo, vol. 1 (January, 2001), ASME, ISBN 9780791878507 [doi]  [abs]
373. Thomas, JP; Dowell, EH; Hall, KC, Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 2001), pp. 230-241, Seattle, WA [doi]  [abs]
374. Thomas, JP; Dowell, EH; Hall, KC, A static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, 39th Aerospace Sciences Meeting and Exhibit (January, 2001) [doi]  [abs]
375. Epureanu, BI; Hall, KC; Dowell, EH, Reduced-order models of unsteady viscous flows in turbomachinery using viscous-inviscid coupling, Journal of Fluids and Structures, vol. 15 no. 2 (January, 2001), pp. 255-273, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
376. Dowell, EH; Thomas, JP; Hall, KC, Transonic limit cycle oscillation analysis using reduced order aerodynamic models, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 2001), pp. 255-263, Seattle, WA [doi]  [abs]
377. Thomas, JP; Dowell, EH; Hall, KC, Three-dimensional transonic aeroelasticity using proper orthogonal decomposition based reduced order models, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 4 (January, 2001), pp. 2555-2564, Seattle, WA [doi]  [abs]
378. Tang, D; Dowell, EH, Effects of angle of attack on nonlinear flutter of a delta wing, Aiaa Journal, vol. 39 no. 1 (January, 2001), pp. 15-21, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
379. Tang, D; Dowell, EH, Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings, Aiaa Journal, vol. 39 no. 8 (January, 2001), pp. 1430-1441, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
380. Tang, D; Kholodar, D; Juang, JN; Dowell, EH, System identification and proper orthogonal decomposition method applied to unsteady aerodynamics, Aiaa Journal, vol. 39 no. 8 (January, 2001), pp. 1569-1576, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
381. Heeg, J; Dowell, EH, Characterizing aeroelastic systems using eigenanalysis, explicitly retaining the aerodynamic degrees of freedom, 19th Aiaa Applied Aerodynamics Conference (January, 2001) [doi]  [abs]
382. Virgin, L. and Trickey, S. and Dowell, E., Stability transitions in a nonlinear airfoil, Proceedings of the 5th Experimental Chaos Conference (2001), pp. 335 - 44, Orlando, FL, USA  [abs]
383. Dowell, EH; Hall, KC, Modeling of fluid-structure interaction, Annual Review of Fluid Mechanics, vol. 33 no. 1 (2001), pp. 445-490, ANNUAL REVIEWS, ISSN 0066-4189 [445], [doi]  [abs]
384. Tang, D; Kholodar, D; Dowell, EH, Nonlinear aeroelastic response of a typical airfoil section with control surface freeplay, 41st Structures, Structural Dynamics, and Materials Conference and Exhibit, vol. 1 no. III (December, 2000), pp. 1514-1523, Atlanta, GA, USA  [abs]
385. Trickey, ST; Virgin, LN; Dowell, EH, Characterizing stability of responses in a nonlinear aeroelastic system, 41st Structures, Structural Dynamics, and Materials Conference and Exhibit, vol. 1 no. I (December, 2000), pp. 57-62, Atlanta, GA, USA  [abs]
386. Tang, D; Dowell, EH, Effects of steady angle of attack on nonlinear flutter of a delta wing plate model, American Society of Mechanical Engineers, Applied Mechanics Division, Amd, vol. 238 (December, 2000), pp. 37-42  [abs]
387. Dowell, EH, Untitled, Aerospace America, vol. 38 no. 9 (September, 2000), pp. 6-6, AMER INST AERONAUT ASTRONAUT, ISSN 0740-722X [Gateway.cgi]
388. Epureanu, BI; Dowell, EH, Optimal multi-dimensional OGY controller, Physica D: Nonlinear Phenomena, vol. 139 no. 1-2 (May, 2000), pp. 87-96, Elsevier BV [S0167-2789(99)00201-8], [doi]  [abs]
389. Clark, RL; Dowell, EH; Frampton, KD, Control of a three-degree-of-freedom airfoil with limit-cycle behavior, Journal of Aircraft, vol. 37 no. 3 (January, 2000), pp. 533-536, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
390. Tang, D; Kholodar, D; Dowell, EH, Nonlinear response of airfoil section with control surface freeplay to gust loads, Aiaa Journal, vol. 38 no. 9 (January, 2000), pp. 1543-1557, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
391. Tang, D; Henry, JK; Dowell, EH, Nonlinear aeroelastic response of delta wing to periodic gust, Journal of Aircraft, vol. 37 no. 1 (January, 2000), pp. 155-164, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
392. Kholodar, DB; Dowell, EH, The Influence of a Nonzero Angle of Attack and Gust Loads on the Nonlinear Response of a Typical Airfoil Section with a Control Surface Freeplay, International Journal of Nonlinear Sciences and Numerical Simulation, vol. 1 no. 3 (January, 2000), pp. 153-165, WALTER DE GRUYTER GMBH [doi]  [abs]
393. Tang, D; Dowell, EH, Effects of steady angle of attack on nonlinear flutter of a delta wing plate model, Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece), vol. 2000-AF (January, 2000), pp. 37-45, ISBN 9780791818978 [doi]  [abs]
394. Tang, D; Kholodar, D; Dowell, EH, Nonlinear aeroelastic response of a typical airfoil section with control surface freeplay, 41st Structures, Structural Dynamics, and Materials Conference and Exhibit, vol. 1 no. III (January, 2000), pp. 1514-1523 [doi]  [abs]
395. Trickey, ST; Virgin, LN; Dowell, EH, Characterizing stability of responses in a nonlinear aeroelastic system, 41st Structures, Structural Dynamics, and Materials Conference and Exhibit, vol. 1 no. I (January, 2000), pp. 57-62 [doi]  [abs]
396. Epureanu, BI; Dowell, EH; Hall, KC, Reduced-order models of unsteady transonic viscous flows in turbomachinery, Journal of Fluids and Structures, vol. 14 no. 8 (2000), pp. 1215-1234, Elsevier BV [0320], [doi]  [abs]
397. Hall Kenneth, C; Thomas Jeffrey, P; Dowell Earl, H, Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows, Aiaa Journal, vol. 38 no. 10 (2000), pp. 1853-1862, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
398. Florea, R; Hall, KC; Dowell, EH, Eigenmode analysis and reduced-order modeling of unsteady transonic potential flow around airfoils, Journal of Aircraft, vol. 37 no. 3 (2000), pp. 454-462, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
399. DOWELL, EH; TANG, D, AUTHOR'S REPLY, Journal of Sound and Vibration, vol. 225 no. 4 (August, 1999), pp. 798-800, Elsevier BV, ISSN 0022-460X [Gateway.cgi], [doi]
400. Dowell, EH; Hall, KC; Thomas, JP; Florea, R; Epureanu, BI; Heeg, J, Reduced order models in unsteady aerodynamics, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 1999), pp. 622-637, St. Louis, MO, USA  [abs]
401. Tang, D; Henry, JK; Dowell, EH, Limit cycle oscillations of delta wing models in low subsonic flow, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (January, 1999), pp. 2162-2172, St. Louis, MO, USA  [abs]
402. Heeg, J; Dowell, EH, Aerodynamic and aeroelastic insights using eigenanalysis, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 (January, 1999), pp. 2242-2252, St. Louis, MO, USA  [abs]
403. Virgin, LN; Dowell, EH; Conner, MD, On the evolution of deterministic non-periodic behavior of an airfoil, International Journal of Non Linear Mechanics, vol. 34 no. 3 (January, 1999), pp. 499-514, Elsevier BV, ISSN 0020-7462 [S0020-7462(98)00038-9], [doi]  [abs]
404. Tang, D; Dowell, EH; Hall, KC, Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow, Aiaa Journal, vol. 37 no. 2-3 (January, 1999), pp. 364-371, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [Gateway.cgi], [doi]  [abs]
405. Kholodar, DB; Dowell, EH, Behavior of airfoil with control surface freeplay for nonzero angles of attack, Aiaa Journal, vol. 37 no. 5 (January, 1999), pp. 651-653, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
406. Tang, D; Henry, JK; Dowell, EH, Limit cycle oscillations of delta wing models in low subsonic flow, Aiaa Journal, vol. 37 no. 11 (January, 1999), pp. 1355-1362, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
407. Hall, KC; Thomas, JP; Dowell, EH, Reduced-order modelling of unsteady small-disturbance flows using a frequency-domain proper orthogonal decomposition technique, 37th Aerospace Sciences Meeting and Exhibit (January, 1999) [doi]  [abs]
408. Epureanu, BI; Dowell, EH; Hall, KC, REDUCED ORDER MODELS OF VISCOUS FLOWS IN TURBOMACHINERY USING PROPER ORTHOGONAL DECOMPOSITION, Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece), vol. 1999-N (January, 1999), pp. 205-215, ISBN 9780791816615 [doi]  [abs]
409. Finnveden, S; Dowell, EH; Tang, D, Comments on “The high-frequency response of a plate carrying a concentrated mass/spring system” [and reply], J. Sound Vib. (Uk), vol. 225 no. 4 (1999), pp. 783-800, Elsevier BV, ISSN 0022-460X [2216], [doi]  [abs]
410. Epureanu Bogdan, I; Dowell Earl, H; Hall Kenneth, C, Reduced order models of viscous flows in turbomachinery using proper orthogonal decomposition, American Society of Mechanical Engineers, Fluids Engineering Division (Publication) Fed, vol. 250 (1999), pp. 205-215, Nashville, TN, USA, ISBN 0791816613  [abs]
411. DOWELL, EH, COMMENTS ON THE NONLINEAR VIBRATIONS OF CYLINDRICAL SHELLS, Journal of Fluids and Structures, vol. 12 no. 8 (November, 1998), pp. 1087-1089, Elsevier BV, ISSN 0889-9746 [Gateway.cgi], [doi]
412. Hu, HY; Dowell, EH; Virgin, LN, Stability estimation of high dimensional vibrating systems under state delay feedback control, Journal of Sound and Vibration, vol. 214 no. 3 (July, 1998), pp. 497-511, Elsevier BV [1548], [doi]  [abs]
413. Dowell, EH; Tang, D, The high-frequency response of a plate carrying a concentrated mass/spring system, Journal of Sound and Vibration, vol. 213 no. 5 (June, 1998), pp. 843-863, Elsevier BV [1520], [doi]  [abs]
414. Dowell, E, Doubling research means doubling education, Scientist, vol. 12 no. 5 (March, 1998), ISSN 0890-3670
415. Reynolds, RR; Dowell, EH, The transient response of structures using asymptotic modal analysis, Journal of Applied Mechanics, vol. 65 no. 1 (January, 1998), pp. 258-265, ASME International, ISSN 0021-8936 [doi]  [abs]
416. Vipperman, JS; Clark, RL; Conner, M; Dowell, EH, Experimental active control of a typical section using a trailing-edge flap, Journal of Aircraft, vol. 35 no. 2 (January, 1998), pp. 224-229, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
417. Tang, D; Conner, MD; Dowell, EH, Reduced-order aerodynamic model and its application to a nonlinear aeroelastic system, Journal of Aircraft, vol. 35 no. 2 (January, 1998), pp. 332-338, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
418. Tang, D; Dowell, EH; Virgin, LN, Limit cycle behavior of an airfoil with a control surface, Journal of Fluids and Structures, vol. 12 no. 7 (January, 1998), pp. 839-858, Elsevier BV [0174], [doi]  [abs]
419. Tang, D; Dowell, EH, Unsteady aerodynamic forces and aeroelastic response for external store of an aircraft, Journal of Aircraft, vol. 35 no. 5 (January, 1998), pp. 678-687, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
420. Tang, D; Dowell, EH; Peters, DA, Reduced order aerodynamic models based upon inflow eigenmodes, Journal of the American Helicopter Society, vol. 43 no. 4 (January, 1998), pp. 342-351, American Helicopter Society [doi]  [abs]
421. Epureanu, BI; Dowell, EH, On the optimality of the Ott-Grebogi-Yorke control scheme, Physica D: Nonlinear Phenomena, vol. 116 no. 1-2 (January, 1998), pp. 1-7, Elsevier BV [S0167-2789(97)00252-2], [doi]  [abs]
422. Hu, H; Dowell, EH; Virgin, LN, Resonances of a Harmonically Forced Duffing Oscillator with Time Delay State Feedback, Nonlinear Dynamics, vol. 15 no. 4 (January, 1998), pp. 311-327 [A:1008278526811], [doi]  [abs]
423. Virgin, LN; Todd, MD; Begley, CJ; Trickey, ST; Dowell, EH, Basins of attraction in experimental nonlinear oscillators, International Journal of Bifurcation and Chaos in Applied Sciences and Engineering, vol. 8 no. 3 (1998), pp. 521-533, World Scientific Pub Co Pte Lt [S0218127498000334], [doi]  [abs]
424. Dowell, EH; Hall, KC; Romanowski, MC, Reduced order aerodynamic modeling of how to make CFD useful to an aeroelastician, American Society of Mechanical Engineers, Aerospace Division (Publication) Ad, vol. 53-3 (December, 1997), pp. 149-163, Dallas, TX, USA  [abs]
425. Vipperman, JS; Clark, RL; Conner, M; Dowell, EH, Investigation of the experimental active control of a typical section airfoil using a trailing edge flap, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 1 (January, 1997), pp. 180-189, Kissimmee, FL, USA  [abs]
426. Tang, D; Dowell, EH, Nonlinear rotor aeroelastic analysis with stall and advanced wake dynamics, Journal of Aircraft, vol. 34 no. 5 (January, 1997), pp. 679-687, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
427. Conner, MD; Tang, DM; Dowell, EH; Virgin, LN, Nonlinear behavior of a typical airfoil section with control surface freeplay: A numerical and experimental study, Journal of Fluids and Structures, vol. 11 no. 1 (January, 1997), pp. 89-109, Elsevier BV [0068], [doi]  [abs]
428. Epureanu, BI; Dowell, EH; Montoya, FM, Pattern formation and linear stability analysis in centreless grinding, Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture, vol. 211 no. 8 (January, 1997), pp. 619-625, SAGE Publications, ISSN 0954-4054 [doi]  [abs]
429. Conner, MD; Tang, DM; Dowell, EH; Virgin, LN, Nonlinear aeroelasticity of an airfoil with control surface freeplay, 35th Aerospace Sciences Meeting and Exhibit (January, 1997)  [abs]
430. Epureanu, BI; Dowell, EH, System identification for the Ott-Grebogi-Yorke controller design, Physical Review E Statistical, Nonlinear, and Soft Matter Physics, vol. 56 no. 5 (January, 1997), pp. 5327-5331 [doi]  [abs]
431. Dowell, EH; Hall, KC; Romanowski, MC, Reduced Order Aerodynamic Modeling of How to Make CFD Useful to An Aeroelastician, Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece), vol. 1997-C (January, 1997), pp. 149-163, ISBN 9780791826775 [doi]  [abs]
432. Conner, M. D. and Tang, D. M. and Dowell, E. H. and Virgin, L. N., Nonlinear Behavior of a Typical Airfoil Section with Control Surface Freeplay: A Numerical and Experimental Study, Journal of Fluids and Structures, vol. 11 no. 1 (1997), pp. 89 - [0068]
433. Dowell Earl, H; Hall Kenneth, C; Romanowski Michael, C, Eigenmode analysis in unsteady aerodynamics: reduced order models, Applied Mechanics Reviews, vol. 50 no. 6 (1997), pp. 371-385, ASME International [doi]  [abs]
434. Epureanu, BI; Dowell, EH; Montoya, FM, Pattern formation and linear stability analysis in centreless grinding, Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture, vol. 211 no. B8 (1997), pp. 619-626, ISSN 0954-4054  [abs]
435. Dowell, EH, Comment on energy flow predictions in a structure of rigidly joined beams using receptance theory, Journal of Sound and Vibration, vol. 194 no. 3 (July, 1996), pp. 445-447, Elsevier BV [0368], [doi]  [abs]
436. Conner, MD; Virgin, LN; Dowell, EH, Accurate numerical integration of state-space models for aeroelastic systems with free play, Aiaa Journal, vol. 34 no. 10 (January, 1996), pp. 2202-2205, American Institute of Aeronautics and Astronautics (AIAA) [doi]
437. Smelova-Reynolds, T; Dowell, EH, The role of higher modes in the chaotic motion of the buckled beam - II, International Journal of Non Linear Mechanics, vol. 31 no. 6 SPEC. ISS. (January, 1996), pp. 941-950, Elsevier BV [S0020-7462(96)00115-1], [doi]  [abs]
438. Tang, D; Dowell, EH, Damping prediction for hingeless rotor aeroelastic stability with experimental correlation, Journal of Aircraft, vol. 33 no. 6 (January, 1996), pp. 1071-1078, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
439. Tang, DM; Cizmas, PGA; Dowell, EH, Experiments and analysis for a gust generator in a wind tunnel, Journal of Aircraft, vol. 33 no. 1 (January, 1996), pp. 139-148, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
440. Smelova-Reynolds, T; Dowell, EH, The role of higher modes in the chaotic motion of the buckled beam - I, International Journal of Non Linear Mechanics, vol. 31 no. 6 SPEC. ISS. (January, 1996), pp. 931-939, Elsevier BV [S0020-7462(96)00114-X], [doi]  [abs]
441. Cizmaş, PGA; Tang, D; Dowell, EH, Flow about a slotted cylinder-airfoil combination in a wind tunnel, Journal of Aircraft, vol. 33 no. 4 (January, 1996), pp. 716-721, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
442. Dowell, EH, Eigenmode analysis in unsteady aerodynamics: Reduced-order models, Aiaa Journal, vol. 34 no. 8 (January, 1996), pp. 1578-1583, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
443. Tang, DM; Dowell, EH, Nonlinear response of a non-rotating rotor blade to a periodic gust, Journal of Fluids and Structures, vol. 10 no. 7 (January, 1996), pp. 721-742, Elsevier BV [0050], [doi]  [abs]
444. Frampton, KD; Clark, RL; Dowell, EH, State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading, Journal of Aircraft, vol. 33 no. 4 (January, 1996), pp. 816-822, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
445. Frampton, KD; Clark, RL; Dowell, EH, Active control of panel flutter with piezoelectric transducers, Journal of Aircraft, vol. 33 no. 4 (January, 1996), pp. 768-774, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
446. Tang, DM; Dowell, EH, Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability, Journal of Fluids and Structures, vol. 10 no. 4 (January, 1996), pp. 353-366, Elsevier BV [0023], [doi]  [abs]
447. Romanowski, MC; Dowell, EH, Reduced order Euler equations for unsteady aerodynamic flows: Numerical techniques, 34th Aerospace Sciences Meeting and Exhibit (January, 1996)  [abs]
448. Tang, D. M. and Dowell, E. H., Nonlinear Response of a Non-Rotating Rotor Blade to a Periodic Gust, Journal of Fluids and Structures, vol. 10 no. 7 (1996), pp. 721 - [0050]
449. Gottwald, JA; Virgin, LN; Dowell, EH, Routes to escape from an energy well, Journal of Sound and Vibration, vol. 187 no. 1 (October, 1995), pp. 133-144, Elsevier BV, ISSN 0022-460X [0506], [doi]  [abs]
450. Dowell, E, Science community must reexamine its own 'contract with America', Scientist, vol. 9 no. 4 (February, 1995), ISSN 0890-3670
451. Dowell, EH, Eigenmode analysis in unsteady aerodynamics: Reduced order models, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 4 no. 4 (January, 1995), pp. 2545-2557, New Orleans, LA, USA, ISSN 0273-4508  [abs]
452. Frampton, KD; Clark, RL; Dowell, EH, Active control of panel flutter with linearized potential flow aerodynamics, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 4 no. 4 (January, 1995), pp. 2273-2280, New Orleans, LA, USA, ISSN 0273-4508  [abs]
453. Frampton, KD; Clark, RL; Dowell, EH, State space modeling for aeroelastic panels subject to linearized potential flow aerodynamic loading, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 2 no. 2 (January, 1995), pp. 1183-1189, New Orleans, LA, USA, ISSN 0273-4508  [abs]
454. Tang, DM; Dowell, EH, Experimental investigation of three-dimensional dynamic stall model oscillating in pitch, Journal of Aircraft, vol. 32 no. 5 (January, 1995), pp. 1062-1071, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
455. Tang, DM; Ilgamov, MA; Dowell, EH, Buckling and post-buckling behavior of a pipe subjected to internal pressure, Journal of Applied Mechanics, vol. 62 no. 3 (January, 1995), pp. 595-600, ASME International, ISSN 0021-8936 [Gateway.cgi], [doi]  [abs]
456. Tang, DM; Dowell, EH, Response of a nonrotating rotor blade to lateral turbulence Part II: Experiment, Journal of Aircraft, vol. 32 no. 1 (January, 1995), pp. 154-160, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
457. Epstein, RJ; Srinivasan, R; Dowell, EH, Flutter of an infinitely long panel in a duct, Aiaa Journal, vol. 33 no. 1 (January, 1995), pp. 109-115, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
458. Romanowski, MC; Dowell, EH, Aeroelastic analysis of an airfoil using eigenmode based reduced order unsteady aerodynamics, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 no. 3 (January, 1995), pp. 1863-1870, New Orleans, LA, USA, ISSN 0273-4508  [abs]
459. Tang, DM; Dowell, EH, Damping prediction for a stalled rotor in flap-lag with experimental correlation, Journal of the American Helicopter Society, vol. 40 no. 4 (January, 1995), pp. 79-89, American Helicopter Society [doi]  [abs]
460. Tang, DM; Dowell, EH, Response of a nonrotating rotor blade to lateral turbulence part I: Theory, Journal of Aircraft, vol. 32 no. 1 (January, 1995), pp. 145-153, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
461. Franzoni, LP; Dowell, EH, On the accuracy of modal analysis in reverberant acoustical systems with damping, The Journal of the Acoustical Society of America, vol. 97 no. 1 (January, 1995), pp. 687-690, Acoustical Society of America (ASA), ISSN 0001-4966 [doi]  [abs]
462. Tang, DM; Dowell, EH, Damping prediction for stalled rotor flap-lag stability with experimental correlation, Applied Mechanics Reviews, vol. 48 no. 11/2 (1995), pp. 189, ASME International [doi]  [abs]
463. Epstein, RJ; Srinivasan, R; Dowell, EH, Flutter of an infinitely long panel in a duct, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 no. 3 (December, 1994), pp. 1366-1374, Hilton Head, SC, USA  [abs]
464. Hopkins, MA; Dowell, EH, Limited amplitude panel flutter with a temperature differential, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 3 no. 3 (December, 1994), pp. 1343-1355, Hilton Head, SC, USA  [abs]
465. Romanowski, MC; Dowell, EH, Using eigenmodes to form an efficient Euler based unsteady aerodynamics analysis, American Society of Mechanical Engineers, Aerospace Division (Publication) Ad, vol. 44 (December, 1994), pp. 147-160, Chicago, IL, USA  [abs]
466. Smelova, TV; Dowell, EH, On necessary conditions for chaotic motion of a buckled plate with external excitation in an aerodynamic flow, American Society of Mechanical Engineers, Applied Mechanics Division, Amd, vol. 192 (December, 1994), pp. 327-332, Chicago, IL, USA  [abs]
467. KATZ, AL; DOWELL, EH, FROM SINGLE WELL CHAOS TO CROSS WELL CHAOS: A DETAILED EXPLANATION IN TERMS OF MANIFOLD INTERSECTIONS, International Journal of Bifurcation and Chaos, vol. 04 no. 04 (August, 1994), pp. 933-941, World Scientific Pub Co Pte Lt, ISSN 0218-1274 [Gateway.cgi], [doi]  [abs]
468. Doherty, SM; Dowel, EH, Experimental study of asymptotic modal analysis applied to a rectangular plate with concentrated masses, Journal of Sound and Vibration, vol. 170 no. 5 (March, 1994), pp. 671-681, Elsevier BV [1093], [doi]  [abs]
469. Ilgamov, MA; Tang, DM; Dowell, EH, Flutter and forced response of a cantilevered pipe: the influence of internal pressure and nozzle discharge, Journal of Membrane Science, vol. 86 no. 1-2 (January, 1994), pp. 139-156  [abs]
470. Lyle, KH; Dowell, EH, Acoustic radiation damping of flat rectangular plates subjected to subsonic flows. Part I: Isotropic, Journal of Fluids and Structures, vol. 8 no. 7 (January, 1994), pp. 711-735, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
471. Lyle, KH; Dowell, EH, Acoustic radiation damping of flat rectangular plates subjected to subsonic flows. Part II: Composite, Journal of Fluids and Structures, vol. 8 no. 7 (January, 1994), pp. 737-746, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
472. Ilgamov, MA; Tang, DM; Dowell, EH, Flutter and forced response of a cantilevered pipe: The influence of internal pressure and nozzle discharge, Journal of Fluids and Structures, vol. 8 no. 2 (January, 1994), pp. 139-156, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
473. BAYLY, PV; VIRGIN, LN; GOTTWALD, JA; DOWELL, EH, STABILITY MEASUREMENTS IN NONLINEAR MECHANICAL EXPERIMENTS GUIDED BY DYNAMICAL SYSTEMS THEORY, edited by Thompson, JMT; Bishop, SR, Nonlinearity and Chaos in Engineering Dynamics (January, 1994), pp. 59-70, JOHN WILEY & SONS LTD, ISBN 0-471-94458-0 [Gateway.cgi]
474. Dowell, EH; Murphy, KD; Latz, AL, Simplified predictive criteria for the onset of Chaos, Nonlinear Dynamics, vol. 6 no. 3 (1994), pp. 247-263, Springer Nature [doi]  [abs]
475. Reynolds, RR; Dowell, EH; Tang, D; Virgin, LN, Nonlinear behavior of low aspect ratio panels in subsonic flow: a preliminary study, American Society of Mechanical Engineers, Aerospace Division (Publication) Ad, vol. 33 (December, 1993), pp. 9-12, New Orleans, LA, USA  [abs]
476. Reynolds, RR; Virgin, LN; Dowell, EH, High-dimensional chaos can lead to weak turbulence, Nonlinear Dynamics, vol. 4 no. 6 (December, 1993), pp. 531-546, Springer Nature [doi]  [abs]
477. Tang, DM; Dowell, EH, Comparison of theory and experiment for non-linear flutter and stall response of a helicopter blade, Journal of Sound and Vibration, vol. 165 no. 2 (August, 1993), pp. 251-276, Elsevier BV [1256], [doi]  [abs]
478. Mahajan, AJ; Bakhle, MA; Dowell, EH, Efficient procedure for cascade aeroelastic stability determination using nonlinear, time-marching aerodynamic solvers, Collection of Technical Papers Aiaa/Asme Structures, Structural Dynamics and Materials Conference no. pt 5 (January, 1993), pp. 2856-2866, La Jolla, CA, USA  [abs]
479. Reynolds, RR; Dowell, EH, Nonlinear aeroelastic response of panels, Collection of Technical Papers Aiaa/Asme Structures, Structural Dynamics and Materials Conference no. pt 5 (January, 1993), pp. 2566-2576, La Jolla, CA, USA  [abs]
480. Mahajan, AJ; Kaza, KRV; Dowell, EH, Semi-Empirical model for prediction of unsteady forces on an airfoil with application to flutter, Journal of Fluids and Structures, vol. 7 no. 1 (January, 1993), pp. 87-103, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
481. Tang, DM; Dowell, EH, Nonlinear aeroelasticity in rotorcraft, Mathematical and Computer Modelling, vol. 18 no. 3-4 (January, 1993), pp. 157-184, Elsevier BV, ISSN 0895-7177 [doi]  [abs]
482. Tang, DM; Dowell, EH, Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade, Aiaa Journal, vol. 31 no. 6 (January, 1993), pp. 1133-1142, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
483. Tang, DM; Dowell, EH, Theoretical and experimental study on nonlinear response of a rotor blade to a gust, Applied Mechanics Reviews, vol. 46 no. 11 (January, 1993), pp. S3-S11, ASME International [doi]  [abs]
484. Tang, D. and Dowell, E., Experimental and theo retical study for nonlinear aeroelastic behavior of a flexible rotor blade, Proceedings of the AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (1993), pp. 1324 -, Dallas, TX, USA
485. Dowell, Earl H., Nonlinear aeroelasticity (1993), pp. 213 -
486. Dowell, EH, Nonlinear dynamics and chaos in mechanical systems, International Conference on Fuzzy Theory and Technology Proceedings, Abstracts and Summaries (December, 1992), pp. 7  [abs]
487. Gottwald, JA; Virgin, LN; Dowell, EH, Experimental mimicry of Duffing's equation, Journal of Sound and Vibration, vol. 158 no. 3 (November, 1992), pp. 447-467, Elsevier BV, ISSN 0022-460X [0022-460X(92)90419-X], [doi]  [abs]
488. Dowell, EH, Author's reply, Journal of Sound and Vibration, vol. 152 no. 2 (January, 1992), pp. 373-374, Elsevier BV, ISSN 0022-460X [doi]
489. Tang, DM; Dowell, EH, Chaotic stall response of helicopter rotor in forward flight, Journal of Fluids and Structures, vol. 6 no. 3 (January, 1992), pp. 311-335, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
490. Peretti, LF; Dowell, EH, Study of intensification zones in a rectangular acoustic cavity, Aiaa Journal, vol. 30 no. 5 (January, 1992), pp. 1199-1206, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
491. Higuchi, K; Dowell, EH, Effect of structural damping on flutter of plates with a follower force, Aiaa Journal, vol. 30 no. 3 (January, 1992), pp. 820-825, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
492. Peretti, LF; Dowell, EH, Asymptotic modal analysis of a rectangular acoustic cavity excited by wall vibration, Aiaa Journal, vol. 30 no. 5 (January, 1992), pp. 1191-1198, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
493. Tang, DM; Dowell, EH, Flutter and stall response of a helicopter blade with structural nonlinearity, Journal of Aircraft, vol. 29 no. 5 (January, 1992), pp. 953-960, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
494. Peretti, LF; Dowell, EH, Experimental verification of the asymptotic modal analysis method as applied to a rectangular acoustic cavity excited by structural vibration, Journal of Vibration and Acoustics, vol. 114 no. 4 (January, 1992), pp. 546-554, ASME International, ISSN 1048-9002 [Gateway.cgi], [doi]  [abs]
495. Kubota, Y; Dowell, EH, Asymptotic modal analysis for sound fields of a reverberant chamber, The Journal of the Acoustical Society of America, vol. 92 no. 2 I (January, 1992), pp. 1106-1112 [doi]  [abs]
496. Dowell, EH, Some comments on the 1988 Rayleigh medal lecture. (JSV 133(1), 1-27), Journal of Sound and Vibration, vol. 144 no. 2 (January, 1991), pp. 355-356, ISSN 0022-460X [doi]
497. Dowell, EH, A chaotic scenario, Journal of Sound and Vibration, vol. 144 no. 1 (January, 1991), pp. 179-180, Elsevier BV, ISSN 0022-460X [0022-460X(91)90741-2], [doi]  [abs]
498. Earl, D; Ye, W, Limit cycle oscillation of a fluttering cantilever plate, Aiaa Journal, vol. 29 no. 11 (January, 1991), pp. 1929-1936 [doi]  [abs]
499. Higuchi, K; Dowell, EH, Effect of constant transverse force on chaotic oscillations of sinusoidally excited buckled beam, International Journal of Non Linear Mechanics, vol. 26 no. 3-4 (January, 1991), pp. 419-426, Elsevier BV, ISSN 0020-7462 [0020-7462(91)90071-Z], [doi]  [abs]
500. Tang, DM; Dowell, EH, Comparison of theory and experiment for nonlinear flutter and stall response of a helicopter blade, Annual Forum Proceedings American Helicopter Society (January, 1991), pp. 1413-1425, Phoenix, AZ, USA  [abs]
501. Mahajan, AJ; Dowell, EH; Bliss, DB, Role of artificial viscosity in Euler and Navier-Stokes solvers, Aiaa Journal, vol. 29 no. 4 (January, 1991), pp. 555-559 [doi]  [abs]
502. Mahajan, AJ; Dowell, EH; Bliss, DB, Eigenvalue calculation procedure for an Euler/Navier-Stokes solver with application to flows over airfoils, Journal of Computational Physics, vol. 97 no. 2 (January, 1991), pp. 398-413, Elsevier BV, ISSN 0021-9991 [0021-9991(91)90006-7], [doi]  [abs]
503. Peretti, LF; Dowell, EH, Experimental verification of the Asymptotic Modal Analysis method as applied to a rectangular acoustic cavity excited by structural vibration, American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) Nca, vol. 9 (December, 1990), pp. 1-7, Dallas, TX, USA  [abs]
504. Kubota, Y; Sekimoto, S; Dowell, EH, The high-frequency response of a plate carrying a concentrated mass, Journal of Sound and Vibration, vol. 138 no. 2 (April, 1990), pp. 321-333, Elsevier BV, ISSN 0022-460X [0022-460X(90)90545-B], [doi]  [abs]
505. Dowell, EH, Nonlinear aeroelasticity, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference no. pt 3 (January, 1990), pp. 1497-1509, Long Beach, CA, USA  [abs]
506. Higuchi, K; Dowell, EH, Effect of a structural damping on dynamic stability of a free flexible plate subjected to a follower force, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference no. pt 4 (January, 1990), pp. 1965-1971, Long Beach, CA, USA  [abs]
507. Higuchi, K; Dowell, EH, Dynamic stability of a rectangular plate with four free edges subjected to a follower force, Aiaa Journal, vol. 28 no. 7 (January, 1990), pp. 1300-1305, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
508. Dowell, EH; Virgin, LN, On spatial chaos, asymptotic modal analysis, and turbulence, Journal of Applied Mechanics, vol. 57 no. 4 (January, 1990), pp. 1094-1097, ASME International, ISSN 0021-8936 [Gateway.cgi], [doi]  [abs]
509. Dowell, EH; Katz, AL; Goldman, RL, Static subsonic aeroelastic stability of a shell wrapped around a rigid surface, Aiaa Journal, vol. 28 no. 4 (January, 1990), pp. 732-739, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
510. Dowell, EH, Comment on “Direct component modal synthesis technique for system dynamic analysis”, Aiaa Journal, vol. 28 no. 12 (January, 1990), pp. 2141-2142 [doi]
511. Dowell, EH, Comment on ‘Direct component modal synthesis technique for system dynamic analysis’, Aiaa Journal, vol. 28 no. 12 (January, 1990), pp. 2141, American Institute of Aeronautics and Astronautics (AIAA) [doi]
512. Dowell, E., Nonlinear aeroelasticity, Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference (1990), pp. 1497 -
513. Higuchi, K. and Dowell, E., Effect of a structural damping on dynamic stability of a free flexible plate subjected to a follower force, Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference (1990), pp. 1965 -
514. Higuchi, K; Dowell, EH, Dynamic stability of a completely free plate subjected to a controlled non-conservative follower force, Journal of Sound and Vibration, vol. 132 no. 1 (July, 1989), pp. 115-128, Elsevier BV, ISSN 0022-460X [0022-460X(89)90875-4], [doi]  [abs]
515. Higuchi, K; Dowell, EH, Effects of the Poisson ratio and negative thrust on the dynamic stability of a free plate subjected to a follower force, Journal of Sound and Vibration, vol. 129 no. 2 (March, 1989), pp. 255-269, Elsevier BV, ISSN 0022-460X [0022-460X(89)90581-6], [doi]  [abs]
516. Miyazawa, Y; Dowell, EH, Approach to modeling and estimation for uncertain systems, Journal of Guidance, Control, and Dynamics, vol. 12 no. 5 (January, 1989), pp. 672-680, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
517. Pezeshki, C; Dowell, EH, Generation and analysis of Lyapunov exponents for the buckled beam, International Journal of Non Linear Mechanics, vol. 24 no. 2 (January, 1989), pp. 79-97, Elsevier BV, ISSN 0020-7462 [0020-7462(89)90001-2], [doi]  [abs]
518. Mahajan, AJ; Dowell, EH; Bliss, DB, On the role of artificial viscosity in Navier-Stokes solvers, 9th Computational Fluid Dynamics Conference, 1989 (January, 1989) [doi]  [abs]
519. Tang, DM; Dowell, EH, On the threshold force for chaotic motions for a forced buckled beam, American Society of Mechanical Engineers (Paper), vol. 55 no. 1 (December, 1988), pp. 190-196 [doi]  [abs]
520. Dowell, EH, Bachelor's Booster, Physics Today, vol. 41 no. 12 (December, 1988), pp. 131 [doi]
521. Ferri, AA; Dowell, EH, Frequency domain solutions to multi-degree-of-freedom, dry friction damped systems, Journal of Sound and Vibration, vol. 124 no. 2 (June, 1988), pp. 207-224, Elsevier BV, ISSN 0022-460X [doi]  [abs]
522. Dowell, EH, Chaotic oscillations in mechanical systems, Computational Mechanics, vol. 3 no. 3 (May, 1988), pp. 199-216, Springer Nature America, Inc [doi]  [abs]
523. Dowell, EH; Pezeshki, C, On necessary and sufficient conditions for chaos to occur in Duffing's equation: an Heuristic approach, Journal of Sound and Vibration, vol. 121 no. 2 (March, 1988), pp. 195-200, ISSN 0022-460X [doi]  [abs]
524. Tang, DM; Dowell, EH, Chaotic oscillations of a cantilevered pipe conveying fluid, Journal of Fluids and Structures, vol. 2 no. 3 (January, 1988), pp. 263-283, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
525. Miyazawa, Y; Dowell, EH, Principal coordinate realization of state estimation and its application of order reduction, Journal of Guidance, Control, and Dynamics, vol. 11 no. 3 (January, 1988), pp. 286-288, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
526. Miyazawa, Y; Do Well, EH, An Estimator for Uncertain Output Matrix Systems, Ieee Transactions on Automatic Control, vol. 33 no. 10 (January, 1988), pp. 967-969, Institute of Electrical and Electronics Engineers (IEEE) [7257], [doi]  [abs]
527. Kubota, Y; Dionne, HD; Dowell, EH, Asymptotic modal analysis and statistical energy analysis of an acoustic cavity, Journal of Vibration and Acoustics, vol. 110 no. 3 (January, 1988), pp. 371-376, ASME International [doi]  [abs]
528. Dowell, E, Chaotic oscillations in mechanical systems, Computers & Structures, vol. 30 no. 1-2 (January, 1988), pp. 171-184, Elsevier BV, Washington, DC, USA, ISSN 0045-7949 [0045-7949(88)90225-8], [doi]  [abs]
529. Pezeshki, C; Dowell, EH, On Chaos and fractal behavior in a generalized duffing's system, Physica D: Nonlinear Phenomena, vol. 32 no. 2 (January, 1988), pp. 194-209, Elsevier BV, ISSN 0167-2789 [0167-2789(88)90051-6], [doi]  [abs]
530. Tang, DM; Dowell, EH, On the threshold force for chaotic motions for a forced buckled beam, Journal of Applied Mechanics, vol. 55 no. 1 (January, 1988), pp. 190-196, ASME International [doi]  [abs]
531. Dowell, EH, Unsteady transonic aerodynamics and aeroelasticity, Applied Mechanics Reviews, vol. 41 no. 8 (January, 1988), pp. 299-319, ASME International [doi]  [abs]
532. Tang, D.M. and Dowell, E.H., On the threshold force for chaotic motions for a forced buckled beam, American Society of Mechanical Engineers (Paper) (1988), pp. 7 - 7, Chicago, IL, USA  [abs]
533. Tang, DM; Dowell, EH, On the threshold force for chaotic motions for a forced buckled beam, American Society of Mechanical Engineers (Paper) (1988), pp. WA/APM7-WA/APM7  [abs]
534. Kubota, Y; Dionne, HD; Dowell, EH, ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF AN ACOUSTIC CAVITY., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) Nca, vol. 3 (December, 1987), pp. 27-35, Boston, MA, USA  [abs]
535. Dowell, EH, CLASSICAL MODAL ANALYSIS, ASYMPTOTIC MODAL ANALYSIS, AND STATISTICAL ENERGY ANALYSIS., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) Nca, vol. 3 (December, 1987), pp. 25-26, Boston, MA, USA  [abs]
536. Pezeshki, C; Dowell, EH, An examination of initial condition maps for the sinusoidally excited buckled beam modeled by the Duffing's equation, Journal of Sound and Vibration, vol. 117 no. 2 (September, 1987), pp. 219-232, Elsevier BV, ISSN 0022-460X [0022-460X(87)90535-9], [doi]  [abs]
537. Pierre, C; Dowell, EH, Localization of vibrations by structural irregularity, Journal of Sound and Vibration, vol. 114 no. 3 (May, 1987), pp. 549-564, Elsevier BV, ISSN 0022-460X [doi]  [abs]
538. Dowell, EH, Theory and application of dynamic decoupling in structural analysis: Another view, Finite Elements in Analysis and Design, vol. 3 no. 2 (January, 1987), pp. 119-125, Elsevier BV, ISSN 0168-874X [0168-874X(87)90004-7], [doi]  [abs]
539. Fang, T; Dowell, EH, Numerical simulations of jump phenomena in stable Duffing systems, International Journal of Non Linear Mechanics, vol. 22 no. 3 (January, 1987), pp. 267-274, Elsevier BV, ISSN 0020-7462 [0020-7462(87)90009-6], [doi]  [abs]
540. Fang, T; Dowell, EH, Numerical simulations of periodic and chaotic responses in a stable duffing system, International Journal of Non Linear Mechanics, vol. 22 no. 5 (January, 1987), pp. 401-425, Elsevier BV, ISSN 0020-7462 [0020-7462(87)90033-3], [doi]  [abs]
541. Tang, DM; Dowell, EH, EFFECTS OF NONLINEAR DAMPING IN LANDING GEAR ON HELICOPTER LIMIT CYCLE RESPONSE IN GROUND RESONANCE., Journal of the American Helicopter Society, vol. 32 no. 1 (January, 1987), pp. 45-53 [doi]  [abs]
542. Kubota, Y; Dowell, EH, Asymptotic modal analysis for dynamic stresses of a plate, The Journal of the Acoustical Society of America, vol. 81 no. 5 (January, 1987), pp. 1267-1272, Acoustical Society of America (ASA), ISSN 0001-4966 [Gateway.cgi], [doi]  [abs]
543. Pierre, C; De Man, T; Dowell, EH, Localized vibrations of disordered multispan beams: Theory and experiment, Aiaa Journal, vol. 25 no. 9 (January, 1987), pp. 1249-1257, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
544. Tang, DM; Dowell, EH; Albright, JE, Damping in beams with multiple dry friction supports, Journal of Aircraft, vol. 24 no. 11 (January, 1987), pp. 820-832, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
545. Fang, T; Dowell, EH, TRANSIENT MEAN SQUARE RESPONSE OF RANDOMLY DAMPED LINEAR SYSTEMS., Journal of Sound and Vibration, vol. 113 no. 1 (1987), pp. 71-79, Elsevier BV [doi]  [abs]
546. Dowell, EH, NONLINEAR AEROELASTICITY: AN OVERVIEW., Proceedings of the U.S. National Congress of Applied Mechanics (December, 1986), pp. 171-173, Austin, TX, USA  [abs]
547. Tang, DM; Dowell, EH, Damping in beams and plates due to slipping at the support boundaries, part 2: Numerical and experimental study, Journal of Sound and Vibration, vol. 108 no. 3 (August, 1986), pp. 509-522, Elsevier BV, ISSN 0022-460X [doi]  [abs]
548. Kubota, Y; Dowell, EH, Experimental investigation of asymptotic modal analysis for a rectangular plate, Journal of Sound and Vibration, vol. 106 no. 2 (April, 1986), pp. 203-216, Elsevier BV, ISSN 0022-460X [0022-460X(86)90313-5], [doi]  [abs]
549. Dowell, EH, Damping in beams and plates due to slipping at the support boundaries, Journal of Sound and Vibration, vol. 105 no. 2 (March, 1986), pp. 243-253, Elsevier BV, ISSN 0022-460X [0022-460X(86)90153-7], [doi]  [abs]
550. Tang, DM; Dowell, EH, Influence of nonlinear blade damping on helicopter ground resonance instability, Journal of Aircraft, vol. 23 no. 2 (January, 1986), pp. 104-110, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
551. Dowell, EH; Pezeshki, C, On the understanding of chaos in buffings equation including a comparison with experiment, Journal of Applied Mechanics, vol. 53 no. 1 (January, 1986), pp. 5-9, ASME International, Miami Beach, FL, USA [doi]  [abs]
552. Tang, DM; Dowell, EH, RANDOM RESPONSE OF BEAMS AND PLATES WITH SLIPPING AT SUPPORT BOUNDARIES., Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference no. pt 2 (January, 1986), pp. 411-424, San Antonio, TX, USA [doi]  [abs]
553. Tang, DM; Dowell, EH, Random response of beams and plates with slipping at support boundaries, Aiaa Journal, vol. 24 no. 8 (January, 1986), pp. 1354-1361, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
554. Dowell, E.H. and Pezeshki, C., On the understanding of chaos in Duffings equation including a comparison with experiment, Trans. ASME, J. Appl. Mech. (USA), vol. 53 no. 1 (1986), pp. 5 - 9  [abs]
555. Pierre, C; Ferri, AA; Dowell, EH, MULTI-HARMONIC ANALYSIS OF DRY FRICTION DAMPED SYSTEMS USING AN INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (December, 1985)  [abs]
556. Dowell, EH; Pezeshki, C, ON THE UNDERSTANDING OF CHAOS IN DUFFINGS EQUATION INCLUDING A COMPARISON WITH EXPERIMENT., American Society of Mechanical Engineers (Paper) (December, 1985)  [abs]
557. Moon, FC; Dowell, EH, STRUCTURAL DYNAMICS., American Society of Mechanical Engineers, Applied Mechanics Division, Amd, vol. 70 no. 10 (December, 1985), pp. 1287-1289, ASME International [doi]  [abs]
558. Dowell, EH; Pezeshki, C, ON THE UNDERSTANDING OF CHAOS IN DUFFINGS EQUATION INCLUDING A COMPARISON WITH EXPERIMENT., American Society of Mechanical Engineers (Paper) (December, 1985)  [abs]
559. Dowell, EH, EFFECTS OF COMPLIANT WALLS ON TRANSITION AND TURBULENCE., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) Nca, vol. 1 (December, 1985), pp. 37-52, Miami Beach, FL, USA  [abs]
560. Dowell, EH; Kubota, Y, ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper), vol. 52 no. 4 (December, 1985), pp. 949-949, ASME International [doi]  [abs]
561. Dowell, EH; Kubota, Y, ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper) (December, 1985), pp. 9 -, Miami Beach, FL, USA  [abs]
562. Pierre, C; Ferri, AA; Dowell, EH, MULTI-HARMONIC ANALYSIS OF DRY FRICTION DAMPED SYSTEMS USING AN INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (December, 1985), pp. -, Miami Beach, FL, USA  [abs]
563. Ferri, AA; Dowell, EH, The behavior of a linear, damped modal system with a non-linear spring-mass-dry friction damper system attached, part II, Journal of Sound and Vibration, vol. 101 no. 1 (July, 1985), pp. 55-74, Elsevier BV, ISSN 0022-460X [doi]  [abs]
564. Pierre, C; Ferri, AA; Dowell, EH, Multi-harmonic analysis of dry friction damped systems using an incremental harmonic balance method., Journal of Applied Mechanics, vol. 52 no. 4 , Dec. 1985 (January, 1985), pp. 958-964, ASME International [doi]  [abs]
565. Dowell, EH, The effects of compliant walls on transition and turbulence., In: Shear Flow Structure Interaction Phenomena, Presented at Asme Winter Annual Meeting, (Miami Beach, U.S.A.: Nov. 17 22,, vol. 1 ) (January, 1985), pp. 37-52  [abs]
566. Pierre, C; Dowell, EH, STUDY OF DYNAMIC INSTABILITY OF PLATES BY AN EXTENDED INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper), vol. 52 no. 3 (January, 1985), pp. 693-697  [abs]
567. Pierre, C; Dowell, EH, A study of dynamic instability of plates by an extended incremental harmonic balance method, Journal of Applied Mechanics, vol. 52 no. 3 (January, 1985), pp. 693-697, ASME International, Albuquerque, NM, USA [doi]  [abs]
568. Ueda, T; Dowell, EH, Reply by authors to K. L. Roger, Aiaa Journal, vol. 23 no. 6 (January, 1985), pp. 980, American Institute of Aeronautics and Astronautics (AIAA) [doi]
569. Moon, FC; Dowell, EH, Structural dynamics, Applied Mechanics Reviews, vol. 38 no. 10 (January, 1985), pp. 1287-1289 [doi]  [abs]
570. Pierre, C. and Ferri, A. A. and Dowell, E. H., MULTI-HARMONIC ANALYSIS OF DRY FRICTION DAMPED SYSTEMS USING AN INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (1985), pp. -, Miami Beach, FL, USA  [abs]
571. Dowell, E. H. and Pezeshki, C., ON THE UNDERSTANDING OF CHAOS IN DUFFINGS EQUATION INCLUDING A COMPARISON WITH EXPERIMENT., American Society of Mechanical Engineers (Paper) (1985), pp. 5 -, Miami Beach, FL, USA  [abs]
572. Dowell, E. H. and Kubota, Y., ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper) (1985), pp. 9 -, Miami Beach, FL, USA  [abs]
573. FLUID-STRUCTURE INTERACTION AND AERODYNAMIC DAMPING., edited by Dowell, E. H.;Au-Yang, M. K.; (1985), pp. 230 -, Cincinnati, OH, Engl  [abs]
574. FLUID-STRUCTURE INTERACTION AND AERODYNAMIC DAMPING., edited by Dowell, E. H.;Au-Yang, M. K.; (1985), pp. 230 -, Cincinnati, OH, Engl  [abs]
575. Dowell, EH, On asymptotic approximations to beam model shapes, Journal of Applied Mechanics, vol. 51 no. 2 (January, 1984), pp. 439, ASME International [doi]  [abs]
576. Dowell, EH, Observation and evolution of chaos for an autonomous system, Journal of Applied Mechanics, vol. 51 no. 3 (January, 1984), pp. 664-673, ASME International [doi]  [abs]
577. Dowell, EH, OBSERVATION AND EVOLUTION OF CHAOS FOR AN AUTONOMOUS SYSTEM., American Society of Mechanical Engineers (Paper) (January, 1984), pp. 10 -, New Orleans, LA, USA
578. Ueda, T; Dowell, EH, Doublet-point method for supersonic unsteady lifting surfaces, Aiaa Journal, vol. 22 no. 2 (January, 1984), pp. 179-186, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
579. Ueda, T; Dowell, EH, Flutter analysis using nonlinear aerodynamic forces, Journal of Aircraft, vol. 21 no. 2 (January, 1984), pp. 101-109, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
580. Ueda, T; Dowell, EH, Reply by authors to W.P. Rodden, Aiaa Journal, vol. 22 no. 4 (January, 1984), pp. 575-576, American Institute of Aeronautics and Astronautics (AIAA) [doi]
581. Dowell, EH, NONLINEAR AEROELASTICITY., Advances in the Astronautical Sciences, vol. 50 no. pt 2 (December, 1983), pp. 760-799  [abs]
582. Dowell, EH; Schwartz, HB, Forced response of a cantilever beam with a dry friction damper attached, part I: Theory, Journal of Sound and Vibration, vol. 91 no. 2 (November, 1983), pp. 255-267, Elsevier BV, ISSN 0022-460X [0022-460X(83)90901-X], [doi]  [abs]
583. Dowell, EH; Schwartz, HB, Forced response of a cantilever beam with a dry friction damper attached, part II: Experiment, Journal of Sound and Vibration, vol. 91 no. 2 (November, 1983), pp. 269-291, Elsevier BV, ISSN 0022-460X [0022-460X(83)90902-1], [doi]  [abs]
584. Dowell, EH, The behavior of a linear, damped modal system with a non-linear spring-mass-dry friction damper system attached, Journal of Sound and Vibration, vol. 89 no. 1 (July, 1983), pp. 65-84, Elsevier BV, ISSN 0022-460X [0022-460X(83)90911-2], [doi]  [abs]
585. Dowell, EH; Bland, SR; Williams, MH, Linear/nonlinear behavior in unsteady transonic aerodynamics, Aiaa Journal, vol. 21 no. 1 (January, 1983), pp. 38-46, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
586. Cui, EJ; Dowell, EH, Postbuckling behavior of rectangular orthotropic plates with two free side edges, International Journal of Mechanical Sciences, vol. 25 no. 6 (January, 1983), pp. 429-446, Elsevier BV, ISSN 0020-7403 [0020-7403(83)90057-7], [doi]  [abs]
587. Tongue, BH; Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., American Society of Mechanical Engineers (Paper), vol. 50 no. 1 (January, 1983), pp. 204-209 [doi]  [abs]
588. Tongue, BH; Dowell, EH, Component mode analysis of nonlinear, nonconservative systems, Journal of Applied Mechanics, vol. 50 no. 1 (January, 1983), pp. 204-209, ASME International [doi]  [abs]
589. Dowell, E.H., Nonlinear aeroelasticity, Advances in the Astronautical Sciences, vol.50, pt.1-2. Proceedings on an International Symposium on Engineering Sciences and Mechanics (1983), pp. 760 - 99, Taiwan  [abs]
590. Tongue, BH; Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., American Society of Mechanical Engineers (Paper) (1983), pp. 6, Houston, TX, USA
591. Dowell, EH; Ueda, T; Goorjian, PM, Transient decay times and mean values of unsteady oscillations in transonic flow, Aiaa J. (Usa), vol. 21 no. 12 (1983), pp. 1762-1764, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
592. Dowell, EH, Flutter of a buckled plate as an example of chaotic motion of a deterministic autonomous system, Journal of Sound and Vibration, vol. 85 no. 3 (December, 1982), pp. 333-344, Elsevier BV, ISSN 0022-460X [0022-460X(82)90259-0], [doi]  [abs]
593. Dowell, EH, Component mode analysis of a simple non-linear, non-conservative system, Journal of Sound and Vibration, vol. 80 no. 2 (January, 1982), pp. 233-246, Elsevier BV, ISSN 0022-460X [0022-460X(82)90193-6], [doi]  [abs]
594. Ueda, T; Dowell, EH, A new solution method for lifting surfaces in subsonic flow, Aiaa Journal, vol. 20 no. 3 (January, 1982), pp. 348-355, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
595. Dowell, EH, Crack extension in a double cantilevered beam model, Journal of Applied Physics, vol. 52 no. 8 (December, 1981), pp. 5356-5360, AIP Publishing [1.329394], [doi]  [abs]
596. Dowell, EH, Non-linear oscillator models in bluff body aero-elasticity, Journal of Sound and Vibration, vol. 75 no. 2 (March, 1981), pp. 251-264, Elsevier BV, ISSN 0022-460X [0022-460X(81)90343-6], [doi]  [abs]
597. Dowell, EH; Bland, SR; Williams, MH, LINEAR/NONLINEAR BEHAVIOR IN UNSTEADY TRANSONIC AERODYNAMICS., Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference no. Pt 2, and (January, 1981), pp. 654-670, Atlanta, Ga  [abs]
598. Dowell, EH, Control laws for adaptive wind tunnels, Aiaa Journal, vol. 19 no. 11 (January, 1981), pp. 1486-1488, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
599. Chao, CF; Dowell, EH; Bliss, DB, MODAL ANALYSIS OF INTERIOR NOISE FIELDS., Semiconductor International (January, 1981), pp. 29-56, Hartford, CT, USA  [abs]
600. Dowell, EH; Chao, C-F; Bliss, DB, Absorption material mounted on a moving wall-Fluid/wall boundary condition, J. Acoust. Soc. Am. (Usa), vol. 70 no. 1 (1981), pp. 244-245, Acoustical Society of America (ASA) [doi]  [abs]
601. Dowell, EH, SIMPLE METHOD FOR CONVERTING FREQUENCY-DOMAIN AERODYNAMICS TO THE TIME DOMAIN., Nasa Tech Memo no. 81844 (October, 1980), pp. 39 -  [abs]
602. Dowell, EH; Chao, CF; Bliss, DB, ACOUSTOELASTICITY: REVIEW AND EXTENSION., Ammonia Plant Safety (And Related Facilities), vol. 2 (January, 1980), pp. 377-402, Southampton, Engl  [abs]
603. Dowell, EH, Component mode analysis of nonlinear and nonconservative systems, Journal of Applied Mechanics, vol. 47 no. 1 (January, 1980), pp. 172-176, ASME International [doi]
604. Dowell, EH, Interior noise studies for single- and double-walled cylindrical shells, Journal of Aircraft, vol. 17 no. 9 (January, 1980), pp. 690-699, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
605. Dowell, EH, Master plan for prediction of vehicle interior noise, Aiaa Journal, vol. 18 no. 4 (January, 1980), pp. 353-366, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
606. Dowell, EH, SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION., Aeronautical Quarterly, vol. 31 no. pt 4 (January, 1980), pp. 252-284, Cambridge University Press (CUP) [doi]  [abs]
607. Dowell, EH, SIMPLE METHOD FOR CONVERTING FREQUENCY-DOMAIN AERODYNAMICS TO THE TIME DOMAIN., Nasa Tech Memo (January, 1980)  [abs]
608. Dowell, EH; Williams, MH; Chi, MR, ASSESSMENT OF THEORETICAL MODELS FOR VISCOUS AND TRANSONIC FLOW., Agard Conference Proceedings (January, 1980)  [abs]
609. Dowell, E. H., SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION., Aeronautical Quarterly, vol. 31 no. pt 4 (1980), pp. 252 - 284  [abs]
610. Dowell, EH, Bounds on modal damping by a component modes method using Lagrange multipliers, Trans. Asme, J. Appl. Mech. (Usa), vol. 47 no. 1 (1980), pp. 211-213, ASME International [doi]  [abs]
611. Dowell, EH; Hodges, DH, Comment on `direct solutions for Strum-Liouville systems with discontinuous coefficients' [and reply by D.H. Hodges], Aiaa J. (Usa), vol. 18 no. 6 (1980), pp. 735-736, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
612. Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR AND NONCONSERVATIVE SYSTEMS., Journal of Applied Mechanics, Transactions Asme, vol. 47 no. 1 (1980), pp. 172-176  [abs]
613. Dowell, EH, Flutter of plates and shells in practice. (January, 1979), pp. Karlsruhe-Sess  [abs]
614. Ch'ng, E; Dowell, EH, THEORETICAL ANALYSIS OF NONLINEAR EFFECTS ON THE FLUTTER AND DIVERGENCE OF A TUBE CONVEYING FLUID. (January, 1979), pp. 65-81, San Francisco, CA, USA  [abs]
615. Dowell, EH, On some general properties of combined dynamical systems, Journal of Applied Mechanics, vol. 46 no. 1 (January, 1979), pp. 206-209, ASME International [doi]  [abs]
616. Horikawa, H; Dowell, EH, ELEMENTARY EXPLANATION OF THE FLUTTER MECHANISM WITH ACTIVE FEEDBACK CONTROLS., J Aircr, vol. 16 no. 4 (1979), pp. 225-232  [abs]
617. Horikawa, H; Dowell, EH, An elementary explanation of the flutter mechanism with active feedback controls, J. Aircr. (Usa), vol. 16 no. 4 (1979), pp. 225-232, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
618. Dowell, EH, Comments on non-linear flexural vibrations of a cylindrical shell, Journal of Sound and Vibration, vol. 60 no. 4 (October, 1978), pp. 596-597, Elsevier BV, ISSN 0022-460X [doi]
619. Alexandridis, AA; Dowell, EH; Moon, FC, The coupled response of a dynamic element riding on a continuously supported beam, Journal of Applied Mechanics, vol. 45 no. 4 (January, 1978), pp. 864-870, ASME International [doi]  [abs]
620. Dowell, EH, COMPLIANT WALL, SUPERSONIC WIND TUNNEL., The Aeronautical Journal, vol. 82 no. 814 (January, 1978), pp. 448-451  [abs]
621. Dowell, EH, Reverberation time, absorption, and impedance, The Journal of the Acoustical Society of America, vol. 64 no. 1 (January, 1978), pp. 181-191, Acoustical Society of America (ASA) [doi]  [abs]
622. Horikawa, H; Dowell, EH; Moon, FC, Active feedback control of a beam subjected to a nonconservative force, International Journal of Solids and Structures, vol. 14 no. 10 (January, 1978), pp. 821-839, Elsevier BV, ISSN 0020-7683 [0020-7683(78)90073-2], [doi]  [abs]
623. Dowell, EH, ON SOME GENERAL PROPERTIES OF COMBINED DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper) no. 78 -WA/APM-26 (January, 1978)  [abs]
624. Dowell, E. H., REVERBERATION TIME, ABSORPTION, AND IMPEDANCE., Journal of the Acoustical Society of America, vol. 64 no. 1 (1978), pp. 181 - 191  [abs]
625. Dowell, EH, Comments on "On collapse and flutter phenomena in thin tubes conveying fluid" by D.S. Weaver and M.P. Paidoussis, Journal of Sound and Vibration, vol. 55 no. 2 (November, 1977), pp. 312-314, Elsevier BV, ISSN 0022-460X [0022-460X(77)90605-8], [doi]  [abs]
626. Dowell, EH; Gorman, GF; Smith, DA, Acoustoelasticity: General theory, acoustic natural modes and forced response to sinusoidal excitation, including comparisons with experiment, Journal of Sound and Vibration, vol. 52 no. 4 (June, 1977), pp. 519-542, Elsevier BV, ISSN 0022-460X [0022-460X(77)90368-6], [doi]  [abs]
627. Dowell, EH; Traybar, J; Hodges, DH, An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam, Journal of Sound and Vibration, vol. 50 no. 4 (February, 1977), pp. 533-544, Elsevier BV, ISSN 0022-460X [0022-460X(77)90501-6], [doi]  [abs]
628. Vaicaitis, R; Dowell, EH, Response of space shuttle surface insulation panels to acoustic pressure, Journal of Spacecraft and Rockets, vol. 14 no. 12 (January, 1977), pp. 739-746, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
629. Williams, M. H. and Chi, M. R. and Ventres, C. S. and Dowell, E. H., AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS., AIAA Journal, vol. 15 no. 8 (1977), pp. 1159 - 1166  [abs]
630. Vaicaitis, R. and Dowell, E. H., RESPONSE OF SPACE SHUTTLE SURFACE INSULATION PANELS TO ACOUSTIC PRESSURE., Journal of Spacecraft and Rockets, vol. 14 no. 12 (1977), pp. 739 - 746  [abs]
631. Dowell, EH; Ventres, CS, Flutter of an elastic plate under tension, Aiaa J. (Usa), vol. 15 no. 11 (1977), pp. 1653-1655, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
632. Dowell, EH; Chi, MR, Variable thickness shear layer aerodynamics revisited, Aiaa J. (Usa), vol. 15 no. 5 (1977), pp. 745-747, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
633. Williams, MH; Chi, MR; Ventres, CS; Dowell, EH, AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS., Aiaa Journal, vol. 15 no. 8 (1977), pp. 1159-1166  [abs]
634. Dowell, EH; Chi, MR, Variable thickness shear layer aerodynamics revis ited., Aiaa Journal, vol. 15 no. 5 ,May 1977 (1977), pp. 745-747  [abs]
635. Kornecki, A; Dowell, EH; O'Brien, J, On the aeroelastic instability of two-dimensional panels in uniform incompressible flow, Journal of Sound and Vibration, vol. 47 no. 2 (July, 1976), pp. 163-178, Elsevier BV, ISSN 0022-460X [0022-460X(76)90715-X], [doi]  [abs]
636. DOWELL, EH, AEROELASTICITY OF PLATES AND SHELLS. no. (1975) (January, 1975), pp. 1975  [abs]
637. Dowell, EH, SIMPLIFIED THEORY OF OSCILLATING AIRFOILS IN TRANSONIC FLOW. (January, 1975), pp. 655-679, Tucson, AZ, USA  [abs]
638. McLean, JD; Dowell, EH, Swirling flows between coaxial cylinders with injection by radial jets, Aiaa Journal, vol. 13 no. 11 (January, 1975), pp. 1435-1440 [doi]  [abs]
639. Dowell, EH, Radiation from panels as a source of airframe noise, Aiaa Journal, vol. 13 no. 11 (January, 1975), pp. 1529-1530, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
640. Dowell, EH, Vibration and flutter analysis of reusable surface insulation panels, Journal of Spacecraft and Rockets, vol. 12 no. 1 (January, 1975), pp. 44-50, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
641. Dowell, EH, Dynamic analysis of an elastic plate on a thin, elastic foundation, Journal of Sound and Vibration, vol. 35 no. 3 (August, 1974), pp. 343-360, Elsevier BV, ISSN 0022-460X [doi]  [abs]
642. Dowell, EH, Comments on "Vibrations of point supported plates", Journal of Sound and Vibration, vol. 32 no. 4 (February, 1974), pp. 524, Elsevier BV, ISSN 0022-460X [doi]
643. Yan, MJ; Dowell, EH, Elastic sandwich beam or plate equations equivalent to classical theory, Journal of Applied Mechanics, vol. 41 no. 2 (January, 1974), pp. 526-527, ASME International [doi]  [abs]
644. DOWELL, EH; MCLEAN, JD; AMBROSE, J; SRINIVASAN, AV, AEROELASTIC STABILITY OF CYLINDRICAL SHELLS SUBJECTED TO A ROTATING FLOW., Aiaa Journal, vol. 12 no. 12 (DECEMBER, 1974) (January, 1974), pp. 1644-1651, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
645. Klein, LR; Dowell, EH, Analysis of modal damping by component modes method using lagrange multipliers, Journal of Applied Mechanics, vol. 41 no. 2 (January, 1974), pp. 527-528, ASME International [doi]  [abs]
646. Vaicaitis, R; Dowell, EH; Ventres, CS, Nonlinear panel response by a monte carlo approach, Aiaa Journal, vol. 12 no. 5 (January, 1974), pp. 685-691, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
647. Kalmbach, CF; Dowell, EH; Moon, FC, The suppression of a dynamic instability of an elastic body using feedback control, International Journal of Solids and Structures, vol. 10 no. 3 (January, 1974), pp. 361-381, Elsevier BV, ISSN 0020-7683 [0020-7683(74)90083-3], [doi]  [abs]
648. Moon, F.C. and Dowell, E.H., Dynamic interaction between a linear induction motor and elastic reaction rail, Conference on Linear Electric Machines (1974), pp. 173 - 8, London, UK  [abs]
649. Kalmbach, C.F. and Dowell, E.H. and Moon, F.C., The suppression of a dynamic instability of an elastic body using feedback control, Int. J. Solids Struct. (UK), vol. 10 no. 3 (1974), pp. 361 - 81  [abs]
650. Yan, MJ; Dowell, EH, Elastic sandwich beam or plate equations equivalent to classical theory, Trans. Asme, E, J. Appl. Mech. (Usa), vol. 41 no. 2 (1974), pp. 526-527  [abs]
651. Dowell, EH, Theoretical vibration and flutter studies of point supported panels, Journal of Spacecraft and Rockets, vol. 10 no. 6 (January, 1973), pp. 389-395, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
652. Dowell, EH; Ventres, CS, Derivation of aerodynamic kernel functions, Aiaa Journal, vol. 11 no. 11 (January, 1973), pp. 1586-1588, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
653. Dowell, EH, Aerodynamic boundary layer effects on flutter and damping of plates, Journal of Aircraft, vol. 10 no. 12 (January, 1973), pp. 734-738, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
654. Dowell, E. H. and Ventres, C. S., DERIVATION OF AERODYNAMIC KERNEL FUNCTIONS., AIAA Journal, vol. 11 no. 11 (1973), pp. 1586 - 1588  [abs]
655. Yan, M-J; Dowell, ; H, E, High-damping measurements and a preliminary evaluation of an equation for constrained-layer damping, Aiaa J. (Usa), vol. 11 no. 3 (1973), pp. 388-390, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
656. Dowell, EH, Free vibrations of an arbitrary structure in terms of component modes, Journal of Applied Mechanics, vol. 39 no. 3 (January, 1972), pp. 727-732, ASME International [doi]  [abs]
657. Yan, MJ; Dowell, EH, Governing equations for vibrating constrained-layer damping sandwich plates and beams, Journal of Applied Mechanics, vol. 39 no. 4 (January, 1972), pp. 1041-1046, ASME International [doi]  [abs]
658. Dowell, EH, Cross-hatching as an aeroviscoelastic problem, Aiaa Journal, vol. 10 no. 5 (January, 1972), pp. 701-703, American Institute of Aeronautics and Astronautics (AIAA) [doi]
659. Kalmbach, C.F., Jr. and Dowell, E.H. and Moon, F.C., The application of feedback control to the suppression of a dynamic instability of an elastic body, 13th Internation Congress of Theoretical and Applied Mechanics. Abstracts only (1972), pp. 59 -, Moscow, USSR  [abs]
660. Yan, MJ; Dowell, EH, Governing equations for vibrating constrained-layer damping sandwich plates and beams, Trans. Asme, E, J. Appl. Mech. (Usa), vol. 39 no. 4 (1972), pp. 1041-1046  [abs]
661. Dowell, EH, Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutter, Aiaa Journal, vol. 9 no. 5 (January, 1971), pp. 834-841, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
662. Dowell, EH, Free vibrations of a linear structure with arbitrary support conditions, Journal of Applied Mechanics, vol. 38 no. 3 (January, 1971), pp. 595-600, ASME International [doi]  [abs]
663. Lai, J; Dowell, EH; Tauchert, TR, Propagation of Harmonic Waves in a Composite Elastic Cylinder, The Journal of the Acoustical Society of America, vol. 49 no. 1B (January, 1971), pp. 220-228, Acoustical Society of America (ASA) [doi]  [abs]
664. DOWELL EH,, COMMENTS ON '%'TURBULENCE-INDUCED PLATE VIBRATIONS. AN EVALUATION OF FINITE-AND INFINITE- PLATE MODELS'%', The Journal of the Acoustical Society of America, vol. 49 no. 1 pt 2 (January, 1971), pp. 376-379  [abs]
665. Dowell, EH, Comments on “Turbulence-Induced Plate Vibrations: An Evaluation of Finite- and Infinite-Plate Models” [W. A. Strawderman, J. Acoust. Soc. Amer. 46, 1294–1307 (1969)], The Journal of the Acoustical Society of America, vol. 49 no. 1B (January, 1971), pp. 376, Acoustical Society of America (ASA) [doi]  [abs]
666. Dowell, EH, The hydroelastic stability of a flat plate, Journal of Applied Mechanics, vol. 38 no. 2 (January, 1971), pp. 565, ASME International [doi]
667. Dowell, EH, Comments on `turbulence-induced plate vibrations: An evaluation of finite- and infinite-plate models', J. Acoust. Soc. Am. (Usa), vol. 49 no. 1 (1971), pp. 376  [abs]
668. Lai, J-L; Dowell, EH; Tauchert, TR, Propagation of harmonic waves in a composite elastic cylinder, J. Acoust. Soc. Am. (Usa), vol. 49 no. 1 (1971), pp. 220-228  [abs]
669. Dowell, EH, Panel flutter: A review of the aeroelastic stability of plates and shells, Aiaa Journal, vol. 8 no. 3 (January, 1970), pp. 385-399, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
670. Dowell, EH; Ventres, CS, Flutter of low aspect ratio plates, Aiaa Journal, vol. 8 no. 6 (January, 1970), pp. 1162-1164, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
671. Dowell, EH, Flutter of buckled plates at zero dynamic pressure, Aiaa Journal, vol. 8 no. 3 (January, 1970), pp. 583-584, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
672. Dowell, EH, Fatigue life estimation of fluttering panels, Aiaa Journal, vol. 8 no. 10 (January, 1970), pp. 1879-1881, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
673. Ventres, CS; Dowell, EH, Comparison of theory and experiment for nonlinear flutter of loaded plates, Aiaa Journal, vol. 8 no. 11 (January, 1970), pp. 2022-2030, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
674. Dowell, EH, Noise or flutter or both?, Journal of Sound and Vibration, vol. 11 no. 2 (January, 1970), pp. 159-180, Elsevier BV, ISSN 0022-460X [doi]  [abs]
675. Dowell, EH, Nonlinear flutter of curved plates, II, Aiaa Journal, vol. 8 no. 2 (January, 1970), pp. 259-261, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
676. Dowell, EH, Transmission of Noise from a Turbulent Boundary Layer through a Flexible Plate into a Closed Cavity, The Journal of the Acoustical Society of America, vol. 46 no. 1B (January, 1969), pp. 238-252, Acoustical Society of America (ASA) [doi]  [abs]
677. DOWELL, E, TRANSMISSION OF NOISE FROM A TURBULENT BOUNDARY LAYER THROUGH A FLEXIBLE PLATE INTO A CLOSE CAVITY, Acoustical Soc America J, vol. 46 no. 1 pt 2 (1969), pp. 238-252  [abs]
678. Dowell, EH, Nonlinear flutter of curved plates, Aiaa Journal, vol. 7 no. 3 (1969), pp. 424-431, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
679. Dowell, EH; Ventres, CS, Modal equations for the nonlinear flexural vibrations of a cylindrical shell, International Journal of Solids and Structures, vol. 4 no. 10 (January, 1968), pp. 975-991, Elsevier BV, ISSN 0020-7683 [0020-7683(68)90017-6], [doi]  [abs]
680. Dowell, EH, Theoretical-experimental correlation of plate flutter boundaries at low supersonic speeds, Aiaa Journal, vol. 6 no. 9 (January, 1968), pp. 1810-1811, American Institute of Aeronautics and Astronautics (AIAA) [doi]
681. Dowell, E.H. and Ventres, C.S., Modal equations for the nonlinear flexural vibrations of a cylindrical shell, Int. J. Solids Struct. (UK), vol. 4 no. 10 (1968), pp. 975 - 91  [abs]
682. Dowell, E.H. and Ventres, C.S., Nonlinear flutter of loaded plates, AIAA/ASME Structures, Structural Dynamics and Materials Conference (1968), pp. 11 -  [abs]
683. Dowell, EH, Response of plates to fluid loading, Journal of Sound and Vibration, vol. 6 no. 1 (January, 1967), pp. 164-165, Elsevier BV, ISSN 0022-460X [doi]
684. Widnall, SE; Dowell, EH, Aerodynamic forces on an oscillating cylindrical duct with an internal flow, Journal of Sound and Vibration, vol. 6 no. 1 (January, 1967), pp. 71-85, Elsevier BV, ISSN 0022-460X [0022-460X(67)90159-9], [doi]  [abs]
685. Dowell, EH, On the nonlinear flexural vibrations of rings, Aiaa Journal, vol. 5 no. 8 (January, 1967), pp. 1508-1509, American Institute of Aeronautics and Astronautics (AIAA) [doi]
686. Dowell, EH, On the flutter of multibay panels at low supersonic speeds, Aiaa Journal, vol. 5 no. 5 (January, 1967), pp. 1032-1033, American Institute of Aeronautics and Astronautics (AIAA) [doi]
687. Dowell, E.H., Nonlinear oscillations of fluttering plate -- 2, AIAA Journal, vol. 5 no. 10 (1967), pp. 1856 - 1862  [abs]
688. Dowell, EH, Generalized aerodynamic forces on flexible plate undergoing transient motion, Quarterly of Applied Mathematics, vol. 24 no. 4 (1967), pp. 331-338  [abs]
689. Dowell, EH, Nonlinear analysis of flutter of plates and shells, Asme Fluid Solid Interaction (1967), pp. 160-186  [abs]
690. Dowell, EH, Nonlinear oscillations of a fluttering plate. II, Aiaa J. (Usa), vol. 5 no. 10 (1967), pp. 1856-1862, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
691. Dowell, EH, Comments on “On Dynamic Snap Buckling of Shallow Arches”, Aiaa Journal, vol. 4 no. 10 (January, 1966), pp. 1887-1888, American Institute of Aeronautics and Astronautics (AIAA) [doi]
692. Dowell, EH; Widnall, SE, Generalized aerodynamic forces on oscillating cylindrical shell -- Subsonic and supersonic flow, Aiaa Journal, vol. 4 no. 4 (1966), pp. 607-610, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
693. Dowell, EH, Flutter of infinitely long plates and shells -- 2, Aiaa Journal, vol. 4 no. 9 (1966), pp. 1510-1518, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
694. Dowell, EH, Flutter of infinitely long plates and shells -- 1, Aiaa Journal, vol. 4 no. 8 (1966), pp. 1370-1377, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
695. Dowell, EH, Nonlinear oscillations of fluttering plate, Aiaa Journal, vol. 4 no. 7 (1966), pp. 1267-1275, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
696. Dowell, EH; Voss, HM, Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0, Aiaa Journal, vol. 3 no. 12 (1965), pp. 2292-2304, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
697. Voss, HM; Dowell, EH, Effect of aerodynamic damping on flutter of thin panels, Aiaa Journal, vol. 2 no. 1 (January, 1964), pp. 119-120, American Institute of Aeronautics and Astronautics (AIAA) [doi]
698. Dowell, E, Flutter of multibay panels at high supersonic speeds, Aiaa Journal, vol. 2 no. 10 (1964), pp. 1805-1814, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
699. Dugundji, J; Dowell, E; Perkin, B, Subsonic flutter of panels on continuous elastic foundations, Aiaa Journal, vol. 1 no. 5 (1963), pp. 1146-1154, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
700. Deman Tang and Dowell, E.H., Reduced order model analysis for two-dimensional molecular dynamic chain structure attached to an atomic force microscope, Trans. ASME, J. Dyn. Syst. Meas. Control (USA), vol. 126 no. 3 , pp. 531 - 46 [1.1789969]  [abs]