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Publications of Earl H Dowell     :chronological  combined  bibtex listing:

Papers Published

  1. 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]
  2. Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C., 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 (2006), pp. 2437 - 2449, Portsmouth, VA, United States  [abs]
  3. Attar, P.J. and Dowell, E.H., 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 (2006), pp. 1959 - [1.28838]
  4. 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]
  5. Attar, P.J. and Dowell, E.H. and White, J.R. and Thomas, J.P., Reduced order nonlinear system identification methodology, AIAA J. (USA), vol. 44 no. 8 (2006), pp. 1895 - 904 [1.16221]  [abs]
  6. Tang, D. and Attar, P. and Li, A. and Dowell, E.H., Complex dynamics of a pyranose ring structure molecule attached to an Atomic Force Microscope, Nonlinear Dyn. (Netherlands), vol. 45 no. 3-4 (2006), pp. 283 - 303 [s11071-006-0508-9]  [abs]
  7. Deman Tang and Attar, P. and Dowell, E.H., Flutter/limit cycle oscillation analysis and experiment for wing-store model, AIAA J. (USA), vol. 44 no. 7 (2006), pp. 1662 - 75  [abs]
  8. Attar, P.J. and Dowell, E.H., Stochastic analysis of a nonlinear aeroelastic model using the response surface method, J. Aircr. (USA), vol. 43 no. 4 (2006), pp. 1044 - 52 [1.17525]  [abs]
  9. Thomas, J.P. and Dowell, E.H. and Hall, K.C., Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, J. Aircr. (USA), vol. 43 no. 4 (2006), pp. 865 - 78  [abs]
  10. Liu, L. and Thomas, J.P. and Dowell, E.H. and Attar, P. and Hall, K.C., 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 [026]  [abs]
  11. Tang, D. and Dowell, E.H., Flutter and limit-cycle oscillations for a wing-store model with freeplay, J. Aircr. (USA), vol. 43 no. 2 (2006), pp. 487 - 503  [abs]
  12. Dowell, E.H. and Aiqin Li, Modal reduction of mathematical models of biological molecules, J. Comput. Phys. (USA), vol. 211 no. 1 (2006), pp. 262 - 88 [021]  [abs]
  13. Attar, P.J. and Dowell, E.H., A reduced order system ID approach to the modelling of nonlinear structural behavior in aeroelasticity, J. Fluid Struct. (UK), vol. 21 no. 5-7 (2005), pp. 531 - 42 [012]  [abs]
  14. Li, Aiqin and Dowell, Earl H., 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 (2005), pp. 1801 - 1815, Long Beach, CA, United States  [abs]
  15. Liu, Liping and Dowell, Earl H. and Thomas, Jeffrey P., 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 (2005), pp. 1467 - 1476, Austin, TX, United States  [abs]
  16. Dowell, Earl H. and Epureanu, Bogdan I., Nonlinear: Introduction, Nonlinear Dynamics, vol. 39 no. 1-2 (2005), pp. 1 - [s11071-005-6551-0]
  17. Attar, Peter J. and Dowell, Earl H., 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 (2005), pp. 2318 - 2338, Austin, TX, United States  [abs]
  18. Carlson, Henry A. and Feng, James Q. and Thomas, Jeffrey P. and Kielb, Robert E. and Hall, Kenneth C. and Dowell, Earl H., Computational models for nonlinear aeroelasticity, 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers (2005), pp. 4143 - 4152, Reno, NV, United States  [abs]
  19. Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C. and Denegri Jr., Charles M., 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 (2005), pp. 1457 - 1466, Austin, TX, United States  [abs]
  20. Attar, Peter J. and Dowell, Earl H. and Tang, Deman, 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 (2005), pp. 1394 - 1411, Austin, TX, United States  [abs]
  21. Jianhua Xie and Wangcai Ding and Dowell, E.H. and Virgin, L.N., Hopf-flip bifurcation of high dimensional maps and application to vibro-impact systems, Acta Mech. Sin. (Engl. Ser.) (China), vol. 21 no. 4 (2005), pp. 402 - 10 [s10409-005-0045-7]  [abs]
  22. Kanda, A. and Dowell, E.H., Worst-case gust-response analysis for topical airfoil section with control surface, J. Aircr. (USA), vol. 42 no. 4 (2005), pp. 956 - 62  [abs]
  23. Liping Liu and Dowell, E.H., Harmonic balance approach for an airfoil with a freeplay control surface, AIAA J. (USA), vol. 43 no. 4 (2005), pp. 802 - 15  [abs]
  24. Epureanu, B.I. and Yin, S.-H. and Dowell, E.H., Enhanced nonlinear dynamics for accurate identification of stiffness loss in a thermo-shielding panel, Nonlinear Dyn. (Netherlands), vol. 39 no. 1-2 (2005), pp. 197 - 211 [s11071-005-1926-9]  [abs]
  25. Deman Tang and Aiqin Li and Attar, P. and Dowell, E.H., Reduced order dynamic model for polysaccharides molecule attached to an atomic force microscope, J. Comput. Phys. (USA), vol. 201 no. 2 (2004), pp. 723 - 52 [016]  [abs]
  26. Deman Tang and Dowell, E.H., Dynamic analysis of a protein-ligand molecular chain attached to an atomic force microscope, Trans. ASME. J. Vib. Acoust. (USA), vol. 126 no. 4 (2004), pp. 496 - 513 [1.1804999]  [abs]
  27. Attar, Peter J. and Dowell, Earl H. and White, J.R., 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 (2004), pp. 1986 - 2000, Palm Springs, CA, United States  [abs]
  28. Kholodar, Denis B. and Dowell, Earl H. and Thomas, Jeffrey P. and Hall, Kenneth C., Limit-cycle oscillations of a typical airfoil in transonic flow, Journal of Aircraft, vol. 41 no. 5 (2004), pp. 1067 - 1072  [abs]
  29. 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. 19 no. 1 (2004), pp. 17 - 27 [018]  [abs]
  30. Tang, D.M. and Dowell, E.H., 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 (2004), pp. 291 - 306 [007]  [abs]
  31. Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C. and Denegri Jr., Charles M., 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 (2004), pp. 2044 - 2050, Palm Springs, CA, United States  [abs]
  32. 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]
  33. Thomas, Jeffrey P. and Dowell, Earl H. and 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  [abs]
  34. Tang, D. and Li, A. and Dowell, E.H., Transient response study on rolling effectiveness of multiple control surfaces, Journal of Fluids and Structures, vol. 19 no. 5 (2004), pp. 621 - 634 [006]  [abs]
  35. Kholodar, Denis B. and Dowell, Earl H. and Thomas, Jeffrey P. and Hall, Kenneth C., Improved understanding of transonic flutter: A three-parameter flutter surface, Journal of Aircraft, vol. 41 no. 4 (2004), pp. 911 - 917  [abs]
  36. Liu, L. and Dowell, E.H., The secondary bifurcation of an aeroelastic airfoil motion: effect of high harmonics, Nonlinear Dyn. (Netherlands), vol. 37 no. 1 (2004), pp. 31 - 49 [4d]  [abs]
  37. Tang, D. and Gavin, H.P. and Dowell, E.H., Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 1. Theory, J. Sound Vib. (UK), vol. 269 no. 3-5 (2004), pp. 853 - 74 [S0022-460X(03)00180-9]  [abs]
  38. Tang, D. and Gavin, H.P. and Dowell, E.H., Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 2. Experiment, J. Sound Vib. (UK), vol. 269 no. 3-5 (2004), pp. 875 - 97 [S0022-460X(03)00181-0]  [abs]
  39. Tang, D.M. and Yamamoto, H. and Dowell, E.H., Flutter and limit cycle oscillations of two-dimensional panels in three-dimensional axial flow, Journal of Fluids and Structures, vol. 17 no. 2 (2003), pp. 225 - 242 [S0889-9746(02)00121-4]  [abs]
  40. Attar, P.J. and Dowell, E.H. and Tang, D.M., 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 (2003), pp. 243 - 259 [S0889-9746(02)00123-8]  [abs]
  41. Wilson, T.L. and 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 [J111v39n02_05]  [abs]
  42. Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C., 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 (2003), pp. 289 - 297, Norfolk, VA, United States  [abs]
  43. Tang, Deman and Gavin, Henri P. and Dowell, Earl H., 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 (2003), pp. 1092 - 1108, Norfolk, VA, United States  [abs]
  44. Epureanu, Bogdan I. and Dowell, Earl H., Compact methodology for computing limit-cycle oscillations in aeroelasticity, Journal of Aircraft, vol. 40 no. 5 (2003), pp. 955 - 963  [abs]
  45. Thomas, Jeffrey P. and Hall, Kenneth C. and Dowell, Earl H., 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 (2003), pp. 4779 - 4784, Norfolk, VA, United States  [abs]
  46. Kholodar, Denis B. and Thomas, Jeffrey P. and Dowell, Earl H. and 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  [abs]
  47. Thomas, Jeffrey P. and Dowell, Earl H. and 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  [abs]
  48. Attar, Peter J. and Dowell, Earl H. and Tang, Deman, 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 (2003), pp. 12 - 22, Norfolk, VA, United States  [abs]
  49. Tang, Deman and Dowell, Earl H., 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 (2003), pp. 905 - 924, Washington, DC, United States  [abs]
  50. Dowell, Earl H. and Bliss, Donald B. and Clark, Robert L., Aeroelastic wing with leading- and trailing-edge control surfaces, Journal of Aircraft, vol. 40 no. 3 (2003), pp. 559 - 565  [abs]
  51. Dowell, E.H. and Tang, D., Multiscale, multiphenomena modeling and Simulation at the nanoscale: on constructing reduced-order models for nonlinear dynamical systems with many degrees-of-freedom, Trans. ASME, J. Appl. Mech. (USA), vol. 70 no. 3 (2003), pp. 328 - 38 [1.1558079]  [abs]
  52. Deman Tang and Aiqin Li and Dowell, E.H., Experimental and theoretical study on rolling effectiveness of multiple control surfaces, AIAA J. (USA), vol. 41 no. 2 (2003), pp. 160 - 7  [abs]
  53. Epureanu, B.I. and Dowell, E.H., Localized basis function method for computing limit cycle oscillations, Nonlinear Dyn. (Netherlands), vol. 31 no. 2 (2003), pp. 151 - 66 [A:1022081101766]  [abs]
  54. Epureanu, B.I. and Dowell, E.H. and Hall, K.C., 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 - 87 [1.1511165]  [abs]
  55. Deman Tang and Dowell, E.H., Limit cycle oscillations of two-dimensional panels in low subsonic flow, Int. J. Non-Linear Mech. (UK), vol. 37 no. 7 (2002), pp. 1199 - 209 [S0020-7462(01)00140-8]  [abs]
  56. Kholodar, Denis B. and Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C., 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 (2002), pp. 64 - 79, Denver, CO  [abs]
  57. Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C., A harmonic balance approach for modeling three-dimensional nonlinear unsteady aerodynamics and aeroelasticity, American Society of Mechanical Engineers, Applied Mechanics Division, AMD, vol. 253 no. 2 (2002), pp. 1323 - 1334, New Orleans, LA, United States  [abs]
  58. Reichert, W. Monty and Daniels-Race, Theda and Dowell, Earl H., Time-tested survival skills for a publish or perish environment, Journal of Engineering Education, vol. 91 no. 1 (2002), pp. 133 - 137  [abs]
  59. Tang, Deman and Dowell, Earl H., Limit-cycle hysteresis response for a high-aspect-ratio wing model, Journal of Aircraft, vol. 39 no. 5 (2002), pp. 885 - 888  [abs]
  60. Tang, Deman and Li, Aiqin and Dowell, Earl H., Transient response study on rolling effectiveness of multiple control surfaces, American Society of Mechanical Engineers, Applied Mechanics Division, AMD, vol. 253 no. 1 (2002), pp. 89 - 100, New Orleans, LA, United States  [abs]
  61. Thomas, Jeffrey P. and Dowell, Earl H. and Hall, Kenneth C., 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 (2002), pp. 1658 - 1666, Denver, CO  [abs]
  62. Jer-Nan Juang and Kholodar, D. and Dowell, E.H., System identification of a vortex lattice aerodynamic model, AIAA J. (USA), vol. 40 no. 6 (2002), pp. 1187 - 96, Reno, NV, USA  [abs]
  63. Thomas, J.P. and Dowell, E.H. and Hall, K.C., Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations, AIAA J. (USA), vol. 40 no. 4 (2002), pp. 638 - 46  [abs]
  64. Deman Tang and Dowell, E.H., Experimental and theoretical study of gust response for high-aspect-ratio wing, AIAA J. (USA), vol. 40 no. 3 (2002), pp. 419 - 29  [abs]
  65. Dowell, E.H. and Tang, D., Mathematical model of a nanopaddle oscillator, Journal of Applied Physics, vol. 90 no. 11 (2001), pp. 5606 - [1.1415535]
  66. 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]
  67. Thomas, J.P. and Dowell, E.H. and Hall, K.C., 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 (2001), pp. 230 - 241, Seattle, WA  [abs]
  68. Dowell, E.H. and Thomas, J.P. and Hall, K.C., 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 (2001), pp. 255 - 263, Seattle, WA  [abs]
  69. Thomas, J.P. and Dowell, E.H. and Hall, K.C., 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 (2001), pp. 2555 - 2564, Seattle, WA  [abs]
  70. Tang, D. and Dowell, E.H., Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings, AIAA Journal, vol. 39 no. 8 (2001), pp. 1430 - 1441  [abs]
  71. Dowell, E.H. and Hall, K.C., Modeling of fluid-structure interaction, Annual Review of Fluid Mechanics, vol. 33 (2001), pp. 445 - 490 [445]  [abs]
  72. Deman Tang and Kholodar, D. and Jer-Nan Juang and Dowell, E.H., System identification and proper orthogonal decomposition method applied to unsteady aerodynamics, AIAA J. (USA), vol. 39 no. 8 (2001), pp. 1569 - 76  [abs]
  73. Hall, K.C. and Thomas, J.P. and Dowell, E.H., Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows, AIAA J. (USA), vol. 38 no. 10 (2000), pp. 1853 - 62  [abs]
  74. Kholodar, D.B. and Dowell, E.H., 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, Int. J. Nonlinear Sci. Numer. Simul. (UK), vol. 1 no. 3 (2000), pp. 153 - 65  [abs]
  75. Tang, Deman and Henry, James K. and Dowell, Earl H., Nonlinear aeroelastic response of delta wing to periodic gust, Journal of Aircraft, vol. 37 no. 1 (2000), pp. 155 - 164  [abs]
  76. Florea, Razvan and Hall, Kenneth C. and Dowell, Earl H., Eigenmode analysis and reduced-order modeling of unsteady transonic potential flow around airfoils, Journal of Aircraft, vol. 37 no. 3 (2000), pp. 454 - 462  [abs]
  77. Epureanu, B.I. and Dowell, E.H. and Hall, K.C., Reduced-order models of unsteady transonic viscous flows in turbomachinery, Journal of Fluids and Structures, vol. 14 no. 8 (2000), pp. 1215 - 1234 [0320]  [abs]
  78. Tang, Deman and Dowell, Earl H., 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 (2000), pp. 37 - 42  [abs]
  79. Trickey, Stephen T. and Virgin, Lawrence N. and Dowell, Earl H., Characterizing stability of responses in a nonlinear aeroelastic system, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol. 1 no. I (2000), pp. 57 - 62, Atlanta, GA, USA  [abs]
  80. Tang, Deman and Kholodar, Denis and Dowell, Earl H., Nonlinear response of airfoil section with control surface freeplay to gust loads, AIAA Journal, vol. 38 no. 9 (2000), pp. 1543 - 1557  [abs]
  81. Clark, Robert L. and Dowell, Earl H. and Frampton, Kenneth D., Control of a three-degree-of-freedom airfoil with limit-cycle behavior, Journal of Aircraft, vol. 37 no. 3 (2000), pp. 533 - 536  [abs]
  82. Tang, Deman and Kholodar, Denis and Dowell, Earl H., Nonlinear aeroelastic response of a typical airfoil section with control surface freeplay, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol. 1 no. III (2000), pp. 1514 - 1523, Atlanta, GA, USA  [abs]
  83. Epureanu, B.I. and Dowell, E.H., Optimal multi-dimensional OGY controller, Physica D (Netherlands), vol. 139 no. 1-2 (2000), pp. 87 - 96 [S0167-2789(99)00201-8]  [abs]
  84. Epureanu, Bogdan I. and Dowell, Earl H. and 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  [abs]
  85. Heeg, Jennifer and Dowell, Earl H., Aerodynamic and aeroelastic insights using eigenanalysis, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol. 3 (1999), pp. 2242 - 2252, St. Louis, MO, USA  [abs]
  86. Tang, Deman and Henry, James K. and Dowell, Earl H., 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 (1999), pp. 2162 - 2172, St. Louis, MO, USA  [abs]
  87. Tang, Deman and Henry, James K. and Dowell, Earl H., Limit cycle oscillations of delta wing models in low subsonic flow, AIAA Journal, vol. 37 no. 11 (1999), pp. 1355 - 1362  [abs]
  88. Dowell, Earl H. and Hall, Kenneth C. and Thomas, Jeffrey P. and Florea, Razvan and Epureanu, Bogdan I. and Heeg, Jennifer, Reduced order models in unsteady aerodynamics, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol. 1 (1999), pp. 622 - 637, St. Louis, MO, USA  [abs]
  89. Kholodar, Denis B. and Dowell, Earl H., Behavior of airfoil with control surface freeplay for nonzero angles of attack, AIAA Journal, vol. 37 no. 5 (1999), pp. 651 - 653  [abs]
  90. Tang, Deman and Dowell, Earl H. and Hall, Kenneth C., Limit cycle oscillations of a cantilevered wing in low subsonic flow, AIAA Journal, vol. 37 no. 3 (1999), pp. 364 - 371  [abs]
  91. Finnveden, S. and Dowell, E.H. and 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 [2216]  [abs]
  92. Tang, Deman and Dowell, Earl H. and Peters, David A., Reduced order aerodynamic models based upon inflow eigenmodes, Journal of the American Helicopter Society, vol. 43 no. 4 (1998), pp. 342 - 351  [abs]
  93. Tang, Deman and Dowell, Earl H., Unsteady aerodynamic forces and aeroelastic response for external store of an aircraft, Journal of Aircraft, vol. 35 no. 5 (1998), pp. 678 - 687  [abs]
  94. Virgin, L.N. and Dowell, E.H. and Conner, M.D., On the evolution of deterministic non-periodic behavior of an airfoil, International Journal of Non-Linear Mechanics, vol. 34 no. 3 (1998), pp. 499 - 514 [S0020-7462(98)00038-9]  [abs]
  95. Tang, D. and Dowell, E.H. and Virgin, L.N., Limit cycle behavior of an airfoil with a control surface, Journal of Fluids and Structures, vol. 12 no. 7 (1998), pp. 839 - 858 [0174]  [abs]
  96. Hu, H.Y. and Dowell, E.H. and Virgin, L.N., Stability estimation of high dimensional vibrating systems under state delay feedback control, J. Sound Vib. (UK), vol. 214 no. 3 (1998), pp. 497 - 511 [1548]  [abs]
  97. Dowell, E.H. and Tang, D., The high-frequency response of a plate carrying a concentrated mass/spring system, J. Sound Vib. (UK), vol. 213 no. 5 (1998), pp. 843 - 63 [1520]  [abs]
  98. Epureanu, B.I. and Dowell, E.H., On the optimality of the Ott-Grebogi-Yorke control scheme, Physica D (Netherlands), vol. 116 no. 1-2 (1998), pp. 1 - 7 [S0167-2789(97)00252-2]  [abs]
  99. Haiyan Hu and Dowell, E.H. and Virgin, L.N., Resonances of a harmonically forced Duffing oscillator with time delay state feedback, Nonlinear Dyn. (Netherlands), vol. 15 no. 4 (1998), pp. 311 - 27 [A:1008278526811]  [abs]
  100. Virgin, L.N. and Todd, M.D. and Begley, C.J. and Trickey, S.T. and Dowell, E.H., Basins of attraction in experimental nonlinear oscillators, Int. J. Bifurcation Chaos Appl. Sci. Eng. (Singapore), vol. 8 no. 3 (1998), pp. 521 - 33 [S0218127498000334]  [abs]
  101. Epureanu, B.I. and Dowell, E.H., System identification for the Ott-Grebogi-Yorke controller design, Phys. Rev. E, Stat. Phys. Plasmas Fluids Relat. Interdiscip. Top. (USA), vol. 56 no. 5 (1997), pp. 5327 - 31 [5327]  [abs]
  102. Dowell, Earl H. and Hall, Kenneth C. and Romanowski, Michael C., 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 (1997), pp. 149 - 163, Dallas, TX, USA  [abs]
  103. Vipperman, Jeffrey S. and Clark, Robert L. and Conner, Mark and Dowell, Earl H., 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 & Materials Conference, vol. 1 (1997), pp. 180 - 189, Kissimmee, FL, USA  [abs]
  104. 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 - 109 [0068]  [abs]
  105. 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]
  106. Epureanu, B.I. and Dowell, E.H. and Montoya, F.M., 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  [abs]
  107. Tang, Deman and Dowell, Earl H., Nonlinear rotor aeroelastic analysis with stall and advanced wake dynamics, Journal of Aircraft, vol. 34 no. 5 (1997), pp. 679 - 687  [abs]
  108. Dowell, Earl H. and Hall, Kenneth C. and Romanowski, Michael C., Eigenmode analysis in unsteady aerodynamics: reduced order models, Applied Mechanics Reviews, vol. 50 no. 6 (1997), pp. 371 - 385  [abs]
  109. Smelova-Reynolds, T. and Dowell, E.H., The role of higher modes in the chaotic motion of the buckled beam. I, Int. J. Non-Linear Mech. (UK), vol. 31 no. 6 (1996), pp. 931 - 9 [S0020-7462(96)00114-X]  [abs]
  110. Smelova-Reynolds, T. and Dowell, E.H., The role of higher modes in the chaotic motion of the buckled beam. II, Int. J. Non-Linear Mech. (UK), vol. 31 no. 6 (1996), pp. 941 - 50 [S0020-7462(96)00115-1]  [abs]
  111. Tang, D.M. and Dowell, E.H., Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability, Journal of Fluids and Structures, vol. 10 no. 4 (1996), pp. 353 - 366 [0023]  [abs]
  112. Frampton, Kenneth D. and Clark, Robert L. and Dowell, Earl H., Active control of panel flutter with piezoelectric transducers, Journal of Aircraft, vol. 33 no. 4 (1996), pp. 768 - 774  [abs]
  113. Frampton, Kenneth D. and Clark, Robert L. and Dowell, Earl H., State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading, Journal of Aircraft, vol. 33 no. 4 (1996), pp. 816 - 822  [abs]
  114. 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 - 742 [0050]  [abs]
  115. 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]
  116. Cizmas, Paul G.A. and Tang, Deman and Dowell, Earl H., Flow about a slotted cylinder-airfoil combination in a wind tunnel, Journal of Aircraft, vol. 33 no. 4 (1996), pp. 716 - 721  [abs]
  117. Tang, D.M. and Cizmas, Paul G.A. and Dowell, E.H., Experiments and analysis for a gust generator in a wind tunnel, Journal of Aircraft, vol. 33 no. 1 (1996), pp. 139 - 148  [abs]
  118. Tang, Deman and Dowell, Earl H., Damping prediction for hingeless rotor aeroelastic stability with experimental correlation, Journal of Aircraft, vol. 33 no. 6 (1996), pp. 1071 - 1078  [abs]
  119. Dowell, E.H., Eigenmode analysis in unsteady aerodynamics: reduced-order models, AIAA J. (USA), vol. 34 no. 8 (1996), pp. 1578 - 83  [abs]
  120. Dowell, E.H., Comment on energy flow predictions in a structure of rigidly joined beams using receptance theory, J. Sound Vib. (UK), vol. 194 no. 3 (1996), pp. 445 - 7 [0368]  [abs]
  121. Gottwald, J.A. and Virgin, L.N. and Dowell, E.H., Routes to escape from an energy well, J. Sound Vib. (UK), vol. 187 no. 1 (1995), pp. 133 - 44 [0506]  [abs]
  122. Frampton, Kenneth D. and Clark, Robert L. and Dowell, Earl H., 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 & Materials Conference no. 2 (1995), pp. 1183 - 1189, New Orleans, LA, USA  [abs]
  123. Tang, D.M. and Dowell, E.H., Response of a nonrotating rotor blade to lateral turbulence part I: theory, Journal of Aircraft, vol. 32 no. 1 (1995), pp. 145 - 153  [abs]
  124. Frampton, Kenneth D. and Clark, Robert L. and Dowell, Earl H., Active control of panel flutter with linearized potential flow aerodynamics, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference no. 4 (1995), pp. 2273 - 2280, New Orleans, LA, USA  [abs]
  125. Dowell, Earl H., Eigenmode analysis in unsteady aerodynamics: Reduced order models, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference no. 4 (1995), pp. 2545 - 2557, New Orleans, LA, USA  [abs]
  126. Tang, D.M. and Dowell, E.H., Damping prediction for a stalled rotor in flap-lag with experimental correlation, Journal of the American Helicopter Society, vol. 40 no. 4 (1995), pp. 79 - 89  [abs]
  127. Romanowski, Michael C. and Dowell, Earl H., Aeroelastic analysis of an airfoil using eigenmode based reduced order unsteady aerodynamics, Journal of Engineering and Applied Science no. 3 (1995), pp. 1863 - 1870, New Orleans, LA, USA  [abs]
  128. Epstein, Ronald J. and Srinivasan, Ramakrishna and Dowell, Earl H., Flutter of an infinitely long panel in a duct, AIAA Journal, vol. 33 no. 1 (1995), pp. 109 - 115  [abs]
  129. Tang, D.M. and Dowell, E.H., Response of a nonrotating rotor blade to lateral turbulence part II: experiment, Journal of Aircraft, vol. 32 no. 1 (1995), pp. 154 - 160  [abs]
  130. Tang, D.M. and Dowell, E.H., Experimental investigation of three-dimensional dynamic stall model oscillating in pitch, Journal of Aircraft, vol. 32 no. 5 (1995), pp. 1062 - 1071  [abs]
  131. Tang, D.M. and Dowell, E.H., Damping prediction for stalled rotor flap-lag stability with experimental correlation, Applied Mechanics Reviews, vol. 48 no. 11/2 (1995), pp. 189 -
  132. Franzoni, L.P. and Dowell, E.H., On the accuracy of modal analysis in reverberant acoustical systems with damping, J. Acoust. Soc. Am. (USA), vol. 97 no. 1 (1995), pp. 687 - 90  [abs]
  133. Dowell, E.H. and Murphy, K.D. and Latz, A.L., Simplified predictive criteria for the onset of Chaos, Nonlinear Dynamics, vol. 6 no. 3 (1994), pp. 247 - 263  [abs]
  134. Smelova, Tatyana V. and Dowell, Earl H., 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 (1994), pp. 327 - 332, Chicago, IL, USA  [abs]
  135. Epstein, Ronald J. and Srinivasan, Ramakrishna and Dowell, Earl H., Flutter of an infinitely long panel in a duct, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference no. 3 (1994), pp. 1366 - 1374, Hilton Head, SC, USA  [abs]
  136. Romanowski, Michael C. and Dowell, Earl H., Using eigenmodes to form an efficient Euler based unsteady aerodynamics analysis, American Society of Mechanical Engineers, Aerospace Division (Publication) AD, vol. 44 (1994), pp. 147 - 160, Chicago, IL, USA  [abs]
  137. Hopkins, Mark A. and Dowell, Earl H., Limited amplitude panel flutter with a temperature differential, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Conference no. 3 (1994), pp. 1343 - 1355, Hilton Head, SC, USA  [abs]
  138. Katz, A.L. and Dowell, E.H., From single well chaos to cross well chaos: a detailed explanation in terms of manifold intersections, Int. J. Bifurcation Chaos Appl. Sci. Eng. (Singapore), vol. 4 no. 4 (1994), pp. 933 - 41  [abs]
  139. Doherty, S.M. and Dowell, E.H., Experimental study of asymptotic modal analysis applied to a rectangular plate with concentrated masses, J. Sound Vib. (UK), vol. 170 no. 5 (1994), pp. 671 - 81 [1093]  [abs]
  140. 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
  141. Reynolds, Robert R. and Virgin, Lawrence N. and Dowell, Earl H., High-dimensional chaos cab lead to weak turbulence, Nonlinear Dynamics, vol. 4 no. 6 (1993), pp. 531 - 546  [abs]
  142. Tang, D.M. and Dowell, E.H., 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 (1993), pp. 251 - 276 [1256]  [abs]
  143. Dowell, Earl H., Nonlinear aeroelasticity (1993), pp. 213 -
  144. Reynolds, Robert R. and Dowell, Earl H. and Tang, Deman and Virgin, Lawrence N., Nonlinear behavior of low aspect ratio panels in subsonic flow: a preliminary study, American Society of Mechanical Engineers, Aerospace Division (Publication) AD, vol. 33 (1993), pp. 9 - 12, New Orleans, LA, USA  [abs]
  145. Reynolds, Robert R. and Dowell, Earl H., Nonlinear aeroelastic response of panels, Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference no. pt 5 (1993), pp. 2566 - 2576, La Jolla, CA, USA  [abs]
  146. Mahajan, Aparajit J. and Bakhle, Milind A. and Dowell, Earl H., 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 (1993), pp. 2856 - 2866, La Jolla, CA, USA  [abs]
  147. Tang, D.M. and Dowell, E.H., Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade, AIAA Journal, vol. 31 no. 6 (1993), pp. 1133 - 1142  [abs]
  148. Gottwald, J.A. and Virgin, L.N. and Dowell, E.H., Experimental mimicry of Duffing's equation, J. Sound Vib. (UK), vol. 158 no. 3 (1992), pp. 447 - 67 [0022-460X(92)90419-X]  [abs]
  149. Peretti, L.F. and Dowell, E.H., Experimental verification of the asymptotic modal analysis method as applied to a rectangular acoustic cavity excited by structural vibration, Trans. ASME. J. Vib. Acoust. (USA), vol. 114 no. 4 (1992), pp. 546 - 54  [abs]
  150. Tang, D.M. and Dowell, E.H., Flutter and stall response of a helicopter blade with structural nonlinearity, Journal of Aircraft, vol. 29 no. 5 (1992), pp. 953 - 960  [abs]
  151. Higuchi, Ken and Dowell, Earl H., Effect of structural damping on flutter of plates with a follower force, AIAA Journal, vol. 30 no. 3 (1992), pp. 820 - 825  [abs]
  152. Dowell, E.H., Nonlinear dynamics and chaos in mechanical systems, International Conference on Fuzzy Theory and Technology Proceedings, Abstracts and Summaries (1992), pp. 7 -  [abs]
  153. Kubota, Y. and Dowell, E.H., Asymptotic modal analysis for sound fields of a reverberant chamber, J. Acoust. Soc. Am. (USA), vol. 92 no. 2 (1992), pp. 1106 - 12  [abs]
  154. Peretti, L.F. and Dowell, E.H., Asymptotic modal analysis of a rectangular acoustic cavity excited by wall vibration, AIAA J. (USA), vol. 30 no. 5 (1992), pp. 1191 - 8  [abs]
  155. Peretti, L.F. and Dowell, E.H., Study of intensification zones in a rectangular acoustic cavity, AIAA J. (USA), vol. 30 no. 5 (1992), pp. 1199 - 206  [abs]
  156. Mahajan, A.J. and Dowell, E.H. and Bliss, D.B., Eigenvalue calculation procedure for an Euler/Navier-Stokes solver with application to flows over airfoils, J. Comput. Phys. (USA), vol. 97 no. 2 (1991), pp. 398 - 413 [0021-9991(91)90006-7]  [abs]
  157. Ye Weiliang and Dowell, E., Limit cycle oscillation of a fluttering cantilever plate, AIAA J. (USA), vol. 29 no. 11 (1991), pp. 1929 - 36  [abs]
  158. Tang, D.M. and Dowell, E.H., Comparison of theory and experiment for nonlinear flutter and stall response of a helicopter blade, Annual Forum Proceedings - American Helicopter Society (1991), pp. 1413 - 1425, Phoenix, AZ, USA  [abs]
  159. Higuchi, K. and Dowell, E.H., Effect of constant transverse force on chaotic oscillations of sinusoidally excited buckled beam, Int. J. Non-Linear Mech. (UK), vol. 26 no. 3-4 (1991), pp. 419 - 26 [0020-7462(91)90071-Z]  [abs]
  160. Mahajan, A.J. and Dowell, E.H. and Bliss, D.B., Role of artificial viscosity in Euler and Navier-Stokes solvers, AIAA J. (USA), vol. 29 no. 4 (1991), pp. 555 - 9  [abs]
  161. Dowell, E.H., A chaotic scenario, J. Sound Vib. (UK), vol. 144 no. 1 (1991), pp. 179 - 80 [0022-460X(91)90741-2]  [abs]
  162. Dowell, E.H. and Virgin, L.N., On spatial chaos, asymptotic modal analysis, and turbulence, Trans. ASME, J. Appl. Mech. (USA), vol. 57 no. 4 (1990), pp. 1094 - 7  [abs]
  163. Dowell, E., Nonlinear aeroelasticity, Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference (1990), pp. 1497 -
  164. Dowell, Earl H., Nonlinear aeroelasticity, Collection of Technical Papers - AIAA/ASME/ASCE/AHS Structures, Structural Dynamics & Materials Conference no. pt 3 (1990), pp. 1497 - 1509, Long Beach, CA, USA  [abs]
  165. Higuchi, Ken and Dowell, Earl H., 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 Structures, Structural Dynamics & Materials Conference no. pt 4 (1990), pp. 1965 - 1971, Long Beach, CA, USA  [abs]
  166. 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 -
  167. Peretti, Linda F. and Dowell, Earl H., 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 (1990), pp. 1 - 7, Dallas, TX, USA  [abs]
  168. Higuchi, K. and Dowell, E.H., Dynamic stability of a rectangular plate with four free edges subjected to a follower force, AIAA J. (USA), vol. 28 no. 7 (1990), pp. 1300 - 5  [abs]
  169. Kubota, Y. and Sekimoto, S. and Dowell, E.H., The high-frequency response of a plate carrying a concentrated mass, J. Sound Vib. (UK), vol. 138 no. 2 (1990), pp. 321 - 33 [0022-460X(90)90545-B]  [abs]
  170. Dowell, E.H. and Katz, A.L. and Goldman, R.L., Static subsonic aeroelastic stability of a shell wrapped around a rigid surface, AIAA J. (USA), vol. 28 no. 4 (1990), pp. 732 - 9  [abs]
  171. Pezeshki, C. and Dowell, E.H., Generation and analysis of Lyapunov exponents for the buckled beam, Int. J. Non-Linear Mech. (UK), vol. 24 no. 2 (1989), pp. 79 - 97 [0020-7462(89)90001-2]  [abs]
  172. Higuchi, K. and Dowell, E.H., Dynamic stability of a completely free plate subjected to a controlled non-conservative follower force, J. Sound Vib. (UK), vol. 132 no. 1 (1989), pp. 115 - 28 [0022-460X(89)90875-4]  [abs]
  173. Higuchi, K. and Dowell, E.H., Effects of the Poisson ratio and negative thrust on the dynamic stability of a free plate subjected to a follower force, J. Sound Vib. (UK), vol. 129 no. 2 (1989), pp. 255 - 69 [0022-460X(89)90581-6]  [abs]
  174. Miyazawa, Y. and Dowell, E.H., An estimator for uncertain output matrix systems, IEEE Trans. Autom. Control (USA), vol. 33 no. 10 (1988), pp. 967 - 9 [7257]  [abs]
  175. Dowell, E., Chaotic oscillations in mechanical systems, Comput. Struct. (UK), vol. 30 no. 1-2 (1988), pp. 171 - 84, Washington, DC, USA [0045-7949(88)90225-8]  [abs]
  176. Kubota, Y. and Dionne, H. D. and Dowell, E. H., ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF AN ACOUSTIC CAVITY., Journal of Vibration, Acoustics, Stress, and Reliability in Design, vol. 110 no. 3 (1988), pp. 371 - 376  [abs]
  177. 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]
  178. Ferri, A.A. and Dowell, E.H., Frequency domain solutions to multi-degree-of-freedom, dry friction damped systems, J. Sound Vib. (UK), vol. 124 no. 2 (1988), pp. 207 - 24  [abs]
  179. Miyazawa, Y. and Dowell, E.H., Principal coordinate realization of state estimation and its application to order reduction, J. Guid. Control Dyn. (USA), vol. 11 no. 3 (1988), pp. 286 - 8  [abs]
  180. Tang, D.M. and Dowell, E.H., On the threshold force for chaotic motions for a forced buckled beam, Trans. ASME, J. Appl. Mech. (USA), vol. 55 no. 1 (1988), pp. 190 - 6  [abs]
  181. Dowell, E.H. and Pezeshki, C., On necessary and sufficient conditions for chaos to occur in Duffing's equation: an heuristic approach, J. Sound Vib. (UK), vol. 121 no. 2 (1988), pp. 195 - 200  [abs]
  182. Tang, D. M. and Dowell, E. H. and Albright, J. E., DAMPING IN BEAMS WITH MULTIPLE DRY FRICTION SUPPORTS., Journal of Aircraft, vol. 24 no. 11 (1987), pp. 820 - 832  [abs]
  183. Tang, D. M. and Dowell, Earl H., 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 (1987), pp. 45 - 53  [abs]
  184. Fang, T. and Dowell, E.H., Numerical simulations of periodic and chaotic responses in a stable Duffing system, Int. J. Non-Linear Mech. (UK), vol. 22 no. 5 (1987), pp. 401 - 25 [0020-7462(87)90033-3]  [abs]
  185. Fang, T. and Dowell, E.H., Numerical simulations of jump phenomena in stable Duffing systems, Int. J. Non-Linear Mech. (UK), vol. 22 no. 3 (1987), pp. 267 - 74 [0020-7462(87)90009-6]  [abs]
  186. Dowell, Earl H., THEORY AND APPLICATION OF DYNAMIC DECOUPLING IN STRUCTURAL ANALYSIS: ANOTHER VIEW., Finite Elements in Analysis and Design, vol. 3 no. 2 (1987), pp. 119 - 125 [0168-874X(87)90004-7]  [abs]
  187. Dowell, E. H., CLASSICAL MODAL ANALYSIS, ASYMPTOTIC MODAL ANALYSIS, AND STATISTICAL ENERGY ANALYSIS., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) NCA, vol. 3 (1987), pp. 25 - 26, Boston, MA, USA  [abs]
  188. Kubota, Y. and Dionne, H. D. and Dowell, E. H., 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 (1987), pp. 27 - 35, Boston, MA, USA  [abs]
  189. Kubota, Y. and Dowell, E.H., Asymptotic modal analysis for dynamic stresses of a plate, J. Acoust. Soc. Am. (USA), vol. 81 no. 5 (1987), pp. 1267 - 72  [abs]
  190. Pierre, C. and Dowell, E.H., Localization of vibrations by structural irregularity, J. Sound Vib. (UK), vol. 114 no. 3 (1987), pp. 549 - 64  [abs]
  191. Fang, T. and Dowell, E.H., Transient mean square response of randomly damped linear systems, J. Sound Vib. (UK), vol. 113 no. 1 (1987), pp. 71 - 9  [abs]
  192. Tang, D. M. and Dowell, E. H., RANDOM RESPONSE OF BEAMS AND PLATES WITH SLIPPING AT SUPPORT BOUNDARIES., AIAA Journal, vol. 24 no. 8 (1986), pp. 1354 - 1361  [abs]
  193. Dowell, E. H., NONLINEAR AEROELASTICITY: AN OVERVIEW., Proceedings of the U.S. National Congress of Applied Mechanics (1986), pp. 171 - 173, Austin, TX, USA  [abs]
  194. Tang, D. M. and Dowell, E. H., RANDOM RESPONSE OF BEAMS AND PLATES WITH SLIPPING AT SUPPORT BOUNDARIES., Collection of Technical Papers - AIAA/ASME/ASCE/AHS Structures, Structural Dynamics & Materials Co no. pt 2 (1986), pp. 411 - 424, San Antonio, TX, USA  [abs]
  195. Tang, D. M. and Dowell, E. H., INFLUENCE OF NONLINEAR BLADE DAMPING ON HELICOPTER GROUND RESONANCE INSTABILITY., Journal of Aircraft, vol. 23 no. 2 (1986), pp. 104 - 110  [abs]
  196. Tang, D.M. and Dowell, E.H., Damping in beams and plates due to slipping at the support boundaries. II. Numerical and experimental study, J. Sound Vib. (UK), vol. 108 no. 3 (1986), pp. 509 - 22  [abs]
  197. Kuboita, Y. and Dowell, E.H., Experimental investigation of asymptotic modal analysis for a rectangular plate, J. Sound Vib. (UK), vol. 106 no. 2 (1986), pp. 203 - 16 [0022-460X(86)90313-5]  [abs]
  198. 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]
  199. Dowell, E.H., Damping in beams and plates due to slipping at the support boundaries, J. Sound Vib. (UK), vol. 105 no. 2 (1986), pp. 243 - 53 [0022-460X(86)90153-7]  [abs]
  200. Pierre, C. and Ferri, A.A. and Dowell, E.H., Multi-harmonic analysis of dry friction damped systems using an incremental harmonic balance method, Trans. ASME, J. Appl. Mech. (USA), vol. 52 no. 4 (1985), pp. 958 - 64  [abs]
  201. Dowell, E.H. and Kubota, Y., Asymptotic modal analysis and statistical energy analysis of dynamical systems, Trans. ASME, J. Appl. Mech. (USA), vol. 52 no. 4 (1985), pp. 949 - 57  [abs]
  202. Pierre, C. and Dowell, E. H., STUDY OF DYNAMIC INSTABILITY OF PLATES BY AN EXTENDED INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (1985), pp. 5 -, Albuquerque, NM, USA  [abs]
  203. 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]
  204. 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]
  205. Moon, F. C. and Dowell, E. H., STRUCTURAL DYNAMICS., AMD (Symposia Series) (American Society of Mechanical Engineers, Applied Mechanics Division), vol. 70 (1985), pp. 1287 - 1289  [abs]
  206. 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]
  207. Dowell, E. H., EFFECTS OF COMPLIANT WALLS ON TRANSITION AND TURBULENCE., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) NCA, vol. 1 (1985), pp. 37 - 52, Miami Beach, FL, USA  [abs]
  208. 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]
  209. 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]
  210. 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]
  211. FLUID-STRUCTURE INTERACTION AND AERODYNAMIC DAMPING., edited by Dowell, E. H.;Au-Yang, M. K.; (1985), pp. 230 -, Cincinnati, OH, Engl  [abs]
  212. FLUID-STRUCTURE INTERACTION AND AERODYNAMIC DAMPING., edited by Dowell, E. H.;Au-Yang, M. K.; (1985), pp. 230 -, Cincinnati, OH, Engl  [abs]
  213. Ferri, A.A. and Dowell, E.H., The behavior of a linear, damped modal system with a non-linear spring-mass-dry fraction damper system attached. II, J. Sound Vib. (UK), vol. 101 no. 1 (1985), pp. 55 - 74  [abs]
  214. Ueda, T. and Dowell, E. H., FLUTTER ANALYSIS USING NONLINEAR AERODYNAMIC FORCES., Journal of Aircraft, vol. 21 no. 2 (1984), pp. 101 - 109  [abs]
  215. Dowell, E. H., OBSERVATION AND EVOLUTION OF CHAOS FOR AN AUTONOMOUS SYSTEM., American Society of Mechanical Engineers (Paper) (1984), pp. 10 -, New Orleans, LA, USA
  216. Dowell, E.H., On asymptotic approximations to beam mode shapes, Trans. ASME, J. Appl. Mech. (USA), vol. 51 no. 2 (1984), pp. 439 -  [abs]
  217. Ueda, T. and Dowell, E.H., Doublet-point method for supersonic unsteady lifting surfaces, AIAA J. (USA), vol. 22 no. 2 (1984), pp. 179 - 86  [abs]
  218. Dowell, E.H. and Ueda, T. and Goorjian, P.M., Transient decay times and mean values of unsteady oscillations in transonic flow, AIAA J. (USA), vol. 21 no. 12 (1983), pp. 1762 - 4  [abs]
  219. Dowell, E.H. and Schwartz, H.B., Forced response of a cantilever beam with a dry friction damper attached. II. Experiment, J. Sound Vib. (UK), vol. 91 no. 2 (1983), pp. 269 - 91 [0022-460X(83)90902-1]  [abs]
  220. Dowell, E.H. and Schwartz, H.B., Forced respose of a cantilever beam with a dry friction damper attached. I. Theory, J. Sound Vib. (UK), vol. 91 no. 2 (1983), pp. 255 - 67 [0022-460X(83)90901-X]  [abs]
  221. Cui, E.J. and Dowell, E.H., Postbuckling behavior of rectangular orthotropic plates with two free side edges, Int. J. Mech. Sci. (UK), vol. 25 no. 6 (1983), pp. 429 - 46 [0020-7403(83)90057-7]  [abs]
  222. 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]
  223. Dowell, Earl H., NONLINEAR AEROELASTICITY., Advances in the Astronautical Sciences, vol. 50 no. pt 2 (1983), pp. 760 - 799, Tainan, Taiwan
  224. Tongue, B. H. and Dowell, E. H., COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., American Society of Mechanical Engineers (Paper) (1983), pp. 6 -, Houston, TX, USA
  225. Dowell, E. H., 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 (1983), pp. 65 - 84 [0022-460X(83)90911-2]  [abs]
  226. Tongue, B.H. and Dowell, E.H., Component mode analysis of nonlinear, nonconservative systems, Trans. ASME, J. Appl. Mech. (USA), vol. 50 no. 1 (1983), pp. 204 - 9  [abs]
  227. Dowell, E.H. and Bland, S.R. and Williams, M.H., Linear/nonlinear behavior in unsteady transonic aerodynamics, AIAA J. (USA), vol. 21 no. 1 (1983), pp. 38 - 46  [abs]
  228. Dowell, E.H., Flutter of a buckled plate as an example of chaotic motion of a deterministic autonomous system, J. Sound Vib. (UK), vol. 85 no. 3 (1982), pp. 333 - 44 [0022-460X(82)90259-0]  [abs]
  229. Ueda, T. and Dowell, E. H., NEW SOLUTION METHOD FOR LIFTING SURFACES IN SUBSONIC FLOW., AIAA Journal, vol. 20 no. 3 (1982), pp. 348 - 355  [abs]
  230. Dowell, E.H., Component mode analysis of a simple non-linear, non-conservative system, J. Sound Vib. (UK), vol. 80 no. 2 (1982), pp. 233 - 46 [0022-460X(82)90193-6]  [abs]
  231. Chao, C. F. and Dowell, E. H. and Bliss, D. B., MODAL ANALYSIS OF INTERIOR NOISE FIELDS., Semiconductor International (1981), pp. 29 - 56, Hartford, CT, USA  [abs]
  232. Dowell, Earl H., CONTROL LAWS FOR ADAPTIVE WIND TUNNELS., AIAA Journal, vol. 19 no. 11 (1981), pp. 1486 - 1488  [abs]
  233. Dowell, Earl H. and Bland, Samuel R. and Williams, Marc H., LINEAR/NONLINEAR BEHAVIOR IN UNSTEADY TRANSONIC AERODYNAMICS., Collection of Technical Papers - AIAA/ASME/ASCE/AHS Structures, Structural Dynamics & Materials Conference no. Pt 2, ad (1981), pp. 654 - 670, Atlanta, Ga  [abs]
  234. Dowell, E.H., Crack extension in a double cantilevered beam model, J. Appl. Phys. (USA), vol. 52 no. 8 (1981), pp. 5356 - 60 [1.329394]  [abs]
  235. Dowell, E.H. and Chen-Fu Chao and Bliss, D.B., Absorption material mounted on a moving wall-Fluid/wall boundary condition, J. Acoust. Soc. Am. (USA), vol. 70 no. 1 (1981), pp. 244 - 5  [abs]
  236. Dowell, E.H., Non-linear oscillator models in bluff body aeroelasticity, J. Sound Vib. (UK), vol. 75 no. 2 (1981), pp. 251 - 64 [0022-460X(81)90343-6]  [abs]
  237. Dowell, E.H., A simplified theory of oscillating aerofoils in transonic flow: review and extension, Aeronaut. Q. (UK), vol. 31 (1980), pp. 252 - 84  [abs]
  238. Dowell, Earl H., SIMPLE METHOD FOR CONVERTING FREQUENCY-DOMAIN AERODYNAMICS TO THE TIME DOMAIN., NASA Technical Memorandum no. 81844 (1980), pp. 39 -  [abs]
  239. Dowell, Earl H., MASTER PLAN FOR PREDICTION OF VEHICLE INTERIOR NOISE., AIAA Journal, vol. 18 no. 4 (1980), pp. 353 - 366  [abs]
  240. Dowell, Earl H., INTERIOR NOISE STUDIES FOR SINGLE- AND DOUBLE-WALLED CYLINDRICAL SHELLS., Journal of Aircraft, vol. 17 no. 9 (1980), pp. 690 - 699  [abs]
  241. Dowell, Earl H. and Chao, Chen-fu and Bliss, Donald B., ACOUSTOELASTICITY: REVIEW AND EXTENSION., Ammonia Plant Safety (and Related Facilities), vol. 2 (1980), pp. 377 - 402, Southampton, Engl  [abs]
  242. 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]
  243. Dowell, E.H. and Hodges, D.H., 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 - 6  [abs]
  244. Dowell, E.H., Component mode analysis of nonlinear and nonconservative systems, Trans. ASME, J. Appl. Mech. (USA), vol. 47 no. 1 (1980), pp. 172 - 6
  245. Dowell, E.H., 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 - 13  [abs]
  246. Ch'ng, E. and Dowell, E. H., THEORETICAL ANALYSIS OF NONLINEAR EFFECTS ON THE FLUTTER AND DIVERGENCE OF A TUBE CONVEYING FLUID., IEEE Annual Textile Industry Technical Conference (1979), pp. 65 - 81, San Francisco, CA, USA  [abs]
  247. Horikawa, H. and Dowell, E.H., An elementary explanation of the flutter mechanism with active feedback controls, J. Aircr. (USA), vol. 16 no. 4 (1979), pp. 225 - 32  [abs]
  248. Dowell, E.H., On some general properties of combined dynamical systems, Trans. ASME, J. Appl. Mech. (USA), vol. 46 no. 1 (1979), pp. 206 - 9
  249. Alexandridis, A.A. and Dowell, E.H. and Moon, F.C., The coupled response of a dynamic element riding on the continuously supported beam, Trans. ASME, J. Appl. Mech. (USA), vol. 45 no. 4 (1978), pp. 864 - 70  [abs]
  250. Horikawa, H. and Dowell, E.H. and Moon, F.C., Active feedback control of a beam subjected to a nonconservative force, Int. J. Solids Struct. (UK), vol. 14 no. 10 (1978), pp. 821 - 39 [0020-7683(78)90073-2]  [abs]
  251. Dowell, E. H., REVERBERATION TIME, ABSORPTION, AND IMPEDANCE., Journal of the Acoustical Society of America, vol. 64 no. 1 (1978), pp. 181 - 191  [abs]
  252. Dowell, E. H., COMPLIANT WALL, SUPERSONIC WIND TUNNEL., Aeronautical Journal, vol. 82 no. 814 (1978), pp. 448 - 451  [abs]
  253. Dowell, E.H., Reverberation time, absorption, and impedance, J. Acoust. Soc. Am. (USA), vol. 64 no. 1 (1978), pp. 181 - 91  [abs]
  254. Vaicaitis, R. and Dowell, E.H., Response of Space Shuttle surface insulation panels to acoustic pressure, J. Spacecr. Rockets (USA), vol. 14 no. 12 (1977), pp. 739 - 46  [abs]
  255. Dowell, E.H., Comments on `On collapse and flutter phenomena in thin tubes conveying fluid' by D. S. Weaver and M. P. Paidoussis [and reply], J. Sound Vib. (UK), vol. 55 no. 2 (1977), pp. 312 - 14 [0022-460X(77)90605-8]  [abs]
  256. Dowell, E.H. and Ventres, C.S., Flutter of an elastic plate under tension, AIAA J. (USA), vol. 15 no. 11 (1977), pp. 1653 - 5  [abs]
  257. 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]
  258. 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]
  259. Williams, M.H. and Chi, M.R. and Ventres, C.S. and Dowell, E.H., Aerodynamic effects of inviscid parallel shear flows, AIAA J. (USA), vol. 15 no. 8 (1977), pp. 1159 - 66  [abs]
  260. Dowell, E.H. and Gorman, G.F. and Smith, D.A., Acoustoelasticity: general theory, acoustic natural modes and forced response to sinusoidal excitation, including comparisons with experiment, J. Sound Vib. (UK), vol. 52 no. 4 (1977), pp. 519 - 42 [0022-460X(77)90368-6]  [abs]
  261. Dowell, E.H. and Chi, M.R., Variable thickness shear layer aerodynamics revisited, AIAA J. (USA), vol. 15 no. 5 (1977), pp. 745 - 7  [abs]
  262. Dowell, E.H. and Traybar, J. and Hodges, D.H., An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam, J. Sound Vib. (UK), vol. 50 no. 4 (1977), pp. 533 - 44 [0022-460X(77)90501-6]  [abs]
  263. Kornecki, A. and Dowell, E.H. and O'Brien, J., On the aeroelastic instability of two-dimensional panels in uniform incompressible flow, J. Sound Vib. (UK), vol. 47 no. 2 (1976), pp. 163 - 78 [0022-460X(76)90715-X]  [abs]
  264. McLean, J.D. and Dowell, E.H., Swirling flows between coaxial cylinders with injection by radial jets, AIAA J. (USA), vol. 13 no. 11 (1975), pp. 1435 - 41  [abs]
  265. McLean, J. D. and Dowell, E. H., SWIRLING FLOWS BETWEEN COAXIAL CYLINDERS WITH INJECTION BY RADIAL JETS., AIAA Journal, vol. 13 no. 11 (1975), pp. 1435 - 1440  [abs]
  266. Dowell, Earl H., VIBRATION AND FLUTTER ANALYSIS OF REUSABLE SURFACE INSULATION PANELS., Journal of Spacecraft and Rockets, vol. 12 no. 1 (1975), pp. 44 - 50  [abs]
  267. Dowell, E.H., Aeroelasticity of plates and shells (1975), pp. xiii+139 -  [abs]
  268. Dowell, E. H., RADIATION FROM PANELS AS A SOURCE OF AIRFRAME NOISE., AIAA Journal, vol. 13 no. 11 (1975), pp. 1529 - 1530  [abs]
  269. Dowell, E. H., SIMPLIFIED THEORY OF OSCILLATING AIRFOILS IN TRANSONIC FLOW., Magnetohydrodynamics (English translation of Magnitaya Gidrodinamika) (1975), pp. 655 - 679, Tucson, AZ, USA  [abs]
  270. Dowell, E.H. and Srinivasan, A.V. and McLean, J.D. and Ambrose, J., Aeroelastic stability of cylindrical shells subjected to a rotating flow, AIAA J. (USA), vol. 12 no. 12 (1974), pp. 1644 - 51  [abs]
  271. Kalmbach, Charles F. and Dowell, Earl H. and Moon, Francis C., SUPPRESSION OF A DYNAMIC INSTABILITY OF AN ELASTIC BODY USING FEEDBACK CONTROL., International Journal of Solids and Structures, vol. 10 no. 3 (1974), pp. 361 - 381 [0020-7683(74)90083-3]  [abs]
  272. Vaicaitis, R. and Dowell, E. H. and Ventres, C. S., NONLINEAR PANEL RESPONSE BY A MONTE CARLO APPROACH., AIAA Journal, vol. 12 no. 5 (1974), pp. 685 - 691  [abs]
  273. Klein, L. R. and Dowell, E. H., ANALYSIS OF MODAL DAMPING BY COMPONENT MODES METHOD USING LAGRANGE MULTIPLIERS., Journal of Applied Mechanics, Transactions ASME, vol. 41 Ser E no. 2 (1974), pp. 527 - 528  [abs]
  274. Yan, M. J. and Dowell, E. H., ELASTIC SANDWICH BEAM OR PLATE EQUATIONS EQUIVALENT TO CLASSICAL THEORY., Journal of Applied Mechanics, Transactions ASME, vol. 41 Ser E no. 2 (1974), pp. 526 - 527  [abs]
  275. 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]
  276. Dowell, E.H., Dynamic analysis of an elastic plate on a thin, elastic foundation, J. Sound Vib. (UK), vol. 35 no. 3 (1974), pp. 343 - 60  [abs]
  277. Yan, M.J. and Dowell, E.H., Elastic sandwich beam or plate equations equivalent to classical theory, Trans. ASME, E, J. Appl. Mech. (USA), vol. 41 no. 2 (1974), pp. 526 - 7  [abs]
  278. 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]
  279. Dowell, E.H. and Ventres, C.S., Derivation of aerodynamic kernel functions, AIAA J. (USA), vol. 11 no. 11 (1973), pp. 1586 - 8  [abs]
  280. Dowell, E. H. and Ventres, C. S., DERIVATION OF AERODYNAMIC KERNEL FUNCTIONS., AIAA Journal, vol. 11 no. 11 (1973), pp. 1586 - 1588  [abs]
  281. Dowell, E. H., THEORETICAL VIBRATION AND FLUTTER STUDIES OF POINT SUPPORTED PANELS., Journal of Spacecraft and Rockets, vol. 10 no. 6 (1973), pp. 389 - 395  [abs]
  282. Miin-Jeng Yan and Dowell, E.H., High-damping measurements and a preliminary evaluation of an equation for constrained-layer damping, AIAA J. (USA), vol. 11 no. 3 (1973), pp. 388 - 90  [abs]
  283. Yan, M.-J. and Dowell, E.H., 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 - 6  [abs]
  284. Yan, M. J. and Dowell, E. H., GOVERNING EQUATIONS FOR VIBRATING CONSTRAINED-LAYER DAMPING SANDWICH PLATES AND BEAMS., Journal of Applied Mechanics, Transactions ASME, vol. 39 Ser E no. 4 (1972), pp. 1041 - 1046
  285. Dowell, E. H., FREE VIBRATIONS OF AN ARBITRARY STRUCTURE IN TERMS OF COMPONENT MODES., Journal of Applied Mechanics, Transactions ASME, vol. 39 Ser E no. 3 (1972), pp. 727 - 732
  286. 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]
  287. Jai-Lue Lai and Dowell, E.H. and Tauchert, T.R., Propagation of harmonic waves in a composite elastic cylinder, J. Acoust. Soc. Am. (USA), vol. 49 no. 1 (1971), pp. 220 - 8  [abs]
  288. Dowell, E.H., 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]
  289. Dowell, E.H., Noise or flutter or both?, J. Sound Vib. (UK), vol. 11 no. 2 (1970), pp. 159 - 80  [abs]
  290. Dowell, E.H., Nonlinear flutter of curved plates, AIAA Journal, vol. 7 no. 3 (1969), pp. 424 - 431  [abs]
  291. 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]
  292. Dowell, E.H. and Ventres, C.S., Nonlinear flutter of loaded plates, AIAA/ASME Structures, Structural Dynamics and Materials Conference (1968), pp. 11 -  [abs]
  293. Dowell, E.H. and Ventres, C.S., Modal equations for nonlinear flexural vibrations of cylindrical shell, International Journal of Solids and Structures, vol. 4 no. 10 (1968), pp. 975 - 991 [0020-7683(68)90017-6]  [abs]
  294. Dowell, E.H., Nonlinear oscillations of a fluttering plate. II, AIAA J. (USA), vol. 5 no. 10 (1967), pp. 1856 - 62  [abs]
  295. Widnall, S.E. and Dowell, E.H., Aerodynamic forces on oscillating cylindrical duct with internal flow, Journal of Sound and Vibration, vol. 6 no. 1 (1967), pp. 71 - 85 [0022-460X(67)90159-9]  [abs]
  296. Dowell, E.H., Nonlinear analysis of flutter of plates and shells, ASME -- Fluid-Solid Interaction (1967), pp. 160 - 186  [abs]
  297. Dowell, E.H., Nonlinear oscillations of fluttering plate -- 2, AIAA Journal, vol. 5 no. 10 (1967), pp. 1856 - 1862  [abs]
  298. Dowell, E.H., Generalized aerodynamic forces on flexible plate undergoing transient motion, Quarterly of Applied Mathematics, vol. 24 no. 4 (1967), pp. 331 - 338  [abs]
  299. Dowell, E.H., Nonlinear oscillations of fluttering plate, AIAA Journal, vol. 4 no. 7 (1966), pp. 1267 - 1275  [abs]
  300. Dowell, E.H., Flutter of infinitely long plates and shells -- 1, AIAA Journal, vol. 4 no. 8 (1966), pp. 1370 - 1377  [abs]
  301. Dowell, E.H., Flutter of infinitely long plates and shells -- 2, AIAA Journal, vol. 4 no. 9 (1966), pp. 1510 - 1518  [abs]
  302. Dowell, E.H. and Widnall, S.E., Generalized aerodynamic forces on oscillating cylindrical shell -- Subsonic and supersonic flow, AIAA Journal, vol. 4 no. 4 (1966), pp. 607 - 610  [abs]
  303. Dowell, E.H. and Voss, H.M., 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  [abs]
  304. Dowell, E., Flutter of multibay panels at high supersonic speeds, AIAA Journal, vol. 2 no. 10 (1964), pp. 1805 - 1814  [abs]
  305. Dugundji, J. and Dowell, E. and Perkin, B., Subsonic flutter of panels on continuous elastic foundations, AIAA Journal, vol. 1 no. 5 (1963), pp. 1146 - 1154  [abs]
  306. Pezeshki, C. and Dowell, E.H., An examination of initial condition maps for the sinusoidally excited buckled beam modeled by the Duffing's equation, J. Sound Vib. (UK), vol. 117 no. 2 (8), pp. 219 - 32 [0022-460X(87)90535-9]  [abs]
  307. Trickey, S.T. and Virgin, L.N. and Dowell, E.H., The stability of limit-cycle oscillations in a nonlinear aeroelastic system, Proc. R. Soc. Lond. A, Math. Phys. Eng. Sci. (UK), vol. 458 no. 2025 (8), pp. 2203 - 26 [0965]  [abs]
  308. Li, A. and Dowell, E.H., Asymptotic modal analysis of dynamical systems: the effect of modal cross-correlation, J. Sound Vib. (UK), vol. 276 no. 1-2 (6), pp. 65 - 80 [031]  [abs]
  309. Dowell, E.H., Non-linear theory of unstable plane Poiseuille flow, J. Fluid Mech. (UK), vol. 38 (3), pp. 401 - 14  [abs]
  310. Pierre, C. and De Man Tang and Dowell, E.H., Localized vibrations of disordered multispan beams: theory and experiment, AIAA J. (USA), vol. 25 no. 9 , pp. 1249 - 57  [abs]
  311. Attar, P.J. and Dowell, E.H. and White, J.R., Modeling delta wing limit-cycle oscillations using a high-fidelity structural model, J. Aircr. (USA), vol. 42 no. 5 , pp. 1209 - 17  [abs]
  312. Dowell, E.H., Free vibrations of a linear structure with arbitrary support conditions, Trans. ASME, E, J. Appl. Mech. (USA), vol. 38 no. 3 , pp. 595 - 600  [abs]
  313. Dowell, E.H., Free vibrations of an arbitrary structure in terms of component modes, Trans. ASME, E, J. Appl. Mech. (USA), vol. 39 no. 3 , pp. 727 - 32  [abs]
  314. Pezeshki, C. and Dowell, E.H., On chaos and fractal behavior in a generalized Duffing's system, Physica D (Netherlands), vol. 32 no. 2 , pp. 194 - 209 [0167-2789(88)90051-6]  [abs]
  315. Dowell, E.H. and Tang, D., Nonlinear aeroelasticity and unsteady aerodynamics, AIAA J. (USA), vol. 40 no. 9 , pp. 1697 - 707  [abs]
  316. 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]
  317. Miyazawa, Y. and Dowell, E.H., Approach to modeling and estimation for uncertain systems, J. Guid. Control Dyn. (USA), vol. 12 no. 5 , pp. 672 - 80  [abs]
  318. Dowell, E.H., Observation and evolution of chaos for an autonomous system, Trans. ASME, J. Appl. Mech. (USA), vol. 51 no. 3 , pp. 664 - 73  [abs]
  319. Pierre, C. and Dowell, E.H., A study of dynamic instability of plates by an extended incremental harmonic balance method, Trans. ASME, J. Appl. Mech. (USA), vol. 52 no. 3 , pp. 693 - 7  [abs]
  320. Thomas, J.P. and Hall, K.C. and Dowell, E.H., Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities, AIAA J. (USA), vol. 43 no. 9 , pp. 1931 - 6  [abs]
  321. Tang, D.M. and Ilgamov, M.A. and Dowell, E.H., Buckling and post-buckling behavior of a pipe subjected to internal pressure, Trans. ASME, J. Appl. Mech. (USA), vol. 62 no. 3 , pp. 595 - 600  [abs]