CNCS Center for Nonlinear and Complex Systems
   Search Help Login pdf version printable version

Publications of Kenneth C. Hall    :chronological  alphabetical  by type  bibtex listing:

  1. Hollenbach, R; Kielb, R; Hall, K, Extending a Van Der Pol-Based Reduced-Order Model for Fluid-Structure Interaction Applied to Non-Synchronous Vibrations in Turbomachinery, Journal of Turbomachinery, vol. 144 no. 3 (March, 2022) [doi]  [abs]
  2. Hollenbach, R; Kielb, R; Hall, K, Unsteady Pressure Analysis of an Oscillating Cylinder Exhibiting Non-Synchronous Vibrations, Aiaa Science and Technology Forum and Exposition, Aiaa Scitech Forum 2022 (January, 2022), ISBN 9781624106316 [doi]  [abs]
  3. Hollenbach, R; Kielb, R; Hall, K, Unsteady Pressures Analysis of an Oscillating Airfoil Exhibiting Nonsynchronous Vibrations as Applied to Turbomachinery, Aiaa Science and Technology Forum and Exposition, Aiaa Scitech Forum 2022 (January, 2022), ISBN 9781624106316 [doi]  [abs]
  4. Tedesco, MB; Hall, KC, Blade Vibration and Its Effect on the Optimal Performance of Helicopter Rotors, Journal of Aircraft, vol. 59 no. 1 (January, 2022), pp. 184-195 [doi]  [abs]
  5. Hollenbach, R; Kielb, R; Hall, K, AN IMPROVED PRELIMINARY DESIGN TOOL FOR TURBOMACHINERY BLADES USING VAN DER POL BASED REDUCED-ORDER MODEL FOR NON-SYNCHRONOUS VIBRATIONS, Proceedings of the Asme Turbo Expo, vol. 10-D (January, 2022), ISBN 9780791886120 [doi]  [abs]
  6. Hollenbach, R; Kielb, R; Hall, K, A FLUID-STRUCTURE INTERACTION TOOL USING A VAN DER POL BASED REDUCED-ORDER MODEL FOR BUFFET AND NON-SYNCHRONOUS VIBRATIONS, Proceedings of the Asme Turbo Expo, vol. 10-D no. 1 (January, 2022), ISBN 9780791886120 [doi]  [abs]
  7. Hollenbach, R; Kielb, R; Hall, K, Extending a van der pol based reduced-order model for fluid-structure interaction applied to non-synchronous vibrations in turbomachinery, Proceedings of the Asme Turbo Expo, vol. 2C-2021 (January, 2021), ISBN 9780791884928 [doi]  [abs]
  8. He, L; Hall, KC, ISUAAAT15 Special Issue, Journal of Turbomachinery, vol. 141 no. 10 (October, 2019), ASME International [doi]
  9. Hall, KC; Coutier-Delgosha, O, Special issue on the 17th ISROMAC conference, Journal of Turbomachinery, vol. 141 no. 2 (February, 2019) [doi]
  10. Giovanetti, EB; Hall, KC, Minimum loss load, twist, and chord distributions for coaxial helicopters in hover, Journal of the American Helicopter Society, vol. 62 no. 1 (January, 2017), pp. 1-9, American Helicopter Society [doi]  [abs]
  11. Giovanetti, EB; Hall, KC, Axisymmetric potential flow model of single or coaxial actuator disks, Annual Forum Proceedings Ahs International, vol. 1 (January, 2016), pp. 747-757, ISBN 9781510825062  [abs]
  12. Hall, KC; Marpu, RP; Custer, CH; Venkataramanan, S; Weiss, JM, Comparison of Numerical Methods for the Prediction of Time-Averaged Flow Quantities in a Cooled Multistage Turbine, Asme Turbo Expo 2015: Turbine Technical Conference and Exposition, vol. 2C (June, 2015), pp. V02CT44A028-V02CT44A028, ASME, ISBN 978-0-7918-5665-9 [doi]  [abs]
  13. Giovanetti, EB; Hall, KC, A variational approach to multipoint aerodynamic optimization of conventional and coaxial helicopter rotors, Annual Forum Proceedings Ahs International, vol. 2 no. May (May, 2015), pp. 752-764, ISSN 1552-2938  [abs]
  14. Giovanetti, EB; Hall, KC, Minimum loss load, twist and chord distributions for coaxial helicopters in Hover, Annual Forum Proceedings Ahs International, vol. 1 no. January (January, 2015), pp. 648-657, ISSN 1552-2938  [abs]
  15. Giovanetti, EB; Hall, KC, Optimum design of compound helicopters that use higher harmonic control, Journal of Aircraft, vol. 52 no. 5 (January, 2015), pp. 1444-1453, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669 [doi]  [abs]
  16. Giovanetti, EB; Hall, KC, Optimum design of compound helicopters using higher harmonic control, Annual Forum Proceedings Ahs International, vol. 4 (January, 2014), pp. 2607-2618, ISSN 1552-2938, ISBN 9781632666918  [abs]
  17. Clark, ST; Kielb, RE; Hall, KC, A van der pol based reduced-order model for non-synchronous vibration (NSV) in turbomachinery, Proceedings of the Asme Turbo Expo, vol. 7 B (December, 2013), ASME, ISBN 9780791855270 [doi]  [abs]
  18. Subramanian, V; Custer, CH; Weiss, JM; Hall, KC, Unsteady simulation of a two-stage cooled high pressure turbine using an efficient non-linear harmonic balance method, Proceedings of the Asme Turbo Expo, vol. 6 C (December, 2013), ASME, ISBN 9780791855249 [doi]  [abs]
  19. Hall, KC; Giovanetti, EB, Minimum power requirements and optimal rotor design for conventional and compound helicopters using higher harmonic control, Annual Forum Proceedings Ahs International, vol. 3 (September, 2013), pp. 1867-1883, ISSN 1552-2938  [abs]
  20. 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]
  21. 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]
  22. Ekici, K; Hall, KC; Huang, H; Thomas, JP, Stabilization of explicit flow solvers using a proper-orthogonal- decomposition technique, Aiaa Journal, vol. 51 no. 5 (May, 2013), pp. 1095-1104, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  23. 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]
  24. Lipp, GM; Hall, KC; Mann, BP, Effect of rider position on bicycle stability, Asme International Mechanical Engineering Congress and Exposition, Proceedings (Imece), vol. 4 A (January, 2013), ASME, ISBN 9780791856246 [doi]  [abs]
  25. Ekici, K; Kielb, RE; Hall, KC, The effect of aerodynamic asymmetries on turbomachinery flutter, Journal of Fluids and Structures, vol. 36 (January, 2013), pp. 1-17, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
  26. Custer, CH; Weiss, JM; Subramanian, V; Clark, WS; Hall, KC, Unsteady simulation of a 1.5 stage turbine using an implicitly coupled nonlinear harmonic balance method, Proceedings of the Asme Turbo Expo, vol. 8 no. PARTS A, B, AND C (December, 2012), pp. 2303-2317, ASME, ISBN 9780791844748 [doi]  [abs]
  27. Clark, ST; Kielb, RE; Hall, KC, Developing a reduced-order model to understand nonsynchronous vibration (NSV) in turbomachinery, Proceedings of the Asme Turbo Expo, vol. 7 no. PARTS A AND B (December, 2012), pp. 1373-1382, ASME, ISBN 9780791844731 [doi]  [abs]
  28. Ekici, K; Hall, KC; Huang, H, Stabilization of explicit flow solvers using a proper orthogonal decomposition technique, 50th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, vol. 51 no. 5 (December, 2012), pp. 1095-1104, ISSN 0001-1452 [Gateway.cgi], [doi]  [abs]
  29. 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]
  30. Weiss, JM; Subramanian, V; Hall, KC, Simulation of unsteady turbomachinery flows using an implicitly coupled nonlinear harmonic balance method, Proceedings of the Asme Turbo Expo, vol. 7 no. PARTS A, B, AND C (December, 2011), pp. 1405-1412, ASME, ISBN 9780791854679 [doi]  [abs]
  31. Ekici, K; Hall, KC, Harmonic balance analysis of limit cycle oscillations in turbomachinery, Aiaa Journal, vol. 49 no. 7 (July, 2011), pp. 1478-1487, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
  32. 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]
  33. Hall, KC; Hall, SR, A variational method for computing the optimal aerodynamic performance of conventional and compound helicopters, Annual Forum Proceedings Ahs International, vol. 3 no. 4 (December, 2010), pp. 2767-2784, American Helicopter Society, ISSN 0002-8711 [doi]  [abs]
  34. Ekici, K; Hall, KC, Harmonic balance analysis of limit cycle oscillations in turbomachinery, 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit (December, 2010)  [abs]
  35. Hall, KC; Hall, SR, A variational method for computing the optimal aerodynamic performance of conventional and compound helicopters, Annual Forum Proceedings Ahs International, vol. 1 (November, 2010), pp. 577-594, ISSN 1552-2938  [abs]
  36. Hall, KC; Hall, SR, A variational method for computing the optimal aerodynamic performance of conventional and compound helicopters, Journal of the American Helicopter Society, vol. 55 no. 4 (October, 2010), pp. 0420061-04200616, ISSN 0002-8711 [doi]  [abs]
  37. Ekici, K; Kielb, RE; Hall, KC, Forced response analysis of aerodynamically asymmetric cascades, 46th Aiaa/Asme/Sae/Asee Joint Propulsion Conference and Exhibit (January, 2010) [doi]  [abs]
  38. Ekici, K; Hall, KC; Kielb, RE, Harmonic balance analysis of blade row interactions in a transonic compressor, Journal of Propulsion and Power, vol. 26 no. 2 (January, 2010), pp. 335-343, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0748-4658 [doi]  [abs]
  39. 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]
  40. Hall, KC; Hall, SR, A variational method for computing the optimal aerodynamic performance of conventional and compound helicopters, Annual Forum Proceedings Ahs International, vol. 3 (2010), pp. 2767-2784, ISSN 1552-2938  [abs]
  41. Miyakozawa, T; Kielb, RE; Hall, KC, The Effects of aerodynamic asymmetric perturbations on forced response of bladed disks, Journal of Turbomachinery, vol. 131 no. 4 (October, 2009), pp. 1-8, ASME International, ISSN 0889-504X [doi]  [abs]
  42. Ekici, K; Kielb, RE; Hall, KC, The effect of aerodynamic asymmetries on turbomachinery flutter, 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (January, 2009), ISBN 9781563479694 [doi]  [abs]
  43. Ekici, K; Hall, KC; Kielb, RE, Harmonic balance analysis of forced response in a transonic compressor, 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (January, 2009), ISBN 9781563479694 [doi]  [abs]
  44. Spiker, MA; Kielb, RE; Thomas, JP; Hall, KC, Application of enforced motion to study 2-D cascade lock-in effect, 47th Aiaa Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition (January, 2009), ISBN 9781563479694 [doi]  [abs]
  45. 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]
  46. 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]
  47. 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]
  48. 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]
  49. Ekici, K; Kielb, RE; Hall, KC, Aerodynamic asymmetry analysis of unsteady flows in turbomachinery, Proceedings of the Asme Turbo Expo, vol. 5 no. PART B (December, 2008), pp. 821-834, ASME, ISBN 9780791843154 [doi]  [abs]
  50. Miyakozawa, T; Kielb, RE; Hall, KC, The effects of aerodynamic asymmetric perturbations on forced response of bladed disks, Proceedings of the Asme Turbo Expo, vol. 5 no. PART B (December, 2008), pp. 779-790, ASME, ISBN 9780791843154 [doi]  [abs]
  51. Spiker, MA; Kielb, RE; Hall, KC; Thomas, JP, Efficient design method for non-synchronous vibrations using enforced motion, Proceedings of the Asme Turbo Expo, vol. 5 no. PART B (December, 2008), pp. 735-747, ASME, ISBN 9780791843154 [doi]  [abs]
  52. Ekici, K; Hall, KC, Nonlinear Frequency-Domain Analysis of Unsteady Flows in Turbomachinery with Multiple Excitation Frequencies, Aiaa Journal, vol. 46 no. 8 (August, 2008), pp. 1912-1920, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
  53. 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]
  54. 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]
  55. 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]
  56. Ekici, K; Kielb, RE; Hall, KC, Aerodynamic Asymmetry Analysis of Unsteady Flows in Turbomachinery, Journal of Turbomachinery, vol. 132 no. 1 (2008), pp. 011006-011006, ASME International, ISSN 0889-504X [doi]  [abs]
  57. Thomas, JP; Dowels, EH; Hall, KC; Denegri, CM, Virtual aeroelastic flight testing for the F-16 fighter with stores, Collection of Technical Papers U.S. Air Force T and E Days, 2007(Test and Evaluation (November, 2007), pp. 339-346, ISBN 1563478919  [abs]
  58. Kielb, RE; Hall, KC; Miyakozawa, T, The effect of unsteady aerodynamic asymmetric perturbations on flutter, Proceedings of the Asme Turbo Expo, vol. 5 (September, 2007), pp. 649-654, ASME, ISBN 079184790X [doi]  [abs]
  59. Ekici, K; Hall, KC, Nonlinear analysis of unsteady flows in multistage turbomachines using harmonic balance, Aiaa Journal, vol. 45 no. 5 (May, 2007), pp. 1047-1057, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
  60. Gopinath, AK; Van Der Weide, E; Alonso, JJ; Jameson, A; Ekici, K; Hall, KC, Three-dimensional unsteady multi-stage turbomachinery simulations using the harmonic balance technique, Collection of Technical Papers 45th Aiaa Aerospace Sciences Meeting, vol. 16 (January, 2007), pp. 10753-10772, ISBN 1563478900 [doi]  [abs]
  61. 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]
  62. 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]
  63. Hall, KC, Message from the conference chair, Proceedings of the Asme Turbo Expo, vol. 1 (November, 2006), pp. iii, ISBN 0791842363
  64. Ekici, K; Hall, KC, Fast estimation of unsteady flows in turbomachinery at multiple interblade phase angles, Aiaa J. (Usa), vol. 44 no. 9 (September, 2006), pp. 2136-2142, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [1.23288], [doi]  [abs]
  65. Ekici, K; Hall, KC, Nonlinear frequency-domain analysis of unsteady flows in turbomachinery with multiple excitation frequencies, Collection of Technical Papers Aiaa Applied Aerodynamics Conference, vol. 1 (January, 2006), pp. 623-636, San Francisco, CA, United States, ISSN 1048-5953, ISBN 1563478129 [doi]  [abs]
  66. Ekici, K; Hall, KC, Nonlinear analysis of unsteady flows in multistage turbomachines using the harmonic balance technique, Collection of Technical Papers 44th Aiaa Aerospace Sciences Meeting, vol. 7 (January, 2006), pp. 4920-4933, ISBN 1563478072 [doi]  [abs]
  67. 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]
  68. 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]
  69. 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]
  70. 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]
  71. Kielb, RE; Hall, KC; Hong, E; Pai, SS, Probabilistic flutter analysis of a mistuned bladed disk, Proceedings of the Asme Turbo Expo, vol. 5 PART B (2006), pp. 1145-1150, Barcelona, Spain, ISBN 0791842401  [abs]
  72. 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]
  73. 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]
  74. 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
  75. 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]
  76. Hall, KC; Kielb, RE; Ekici, K; Thomas, JP; Clark, WS, Recent advancements in turbomachinery aeroelastic design analysis, 43rd Aiaa Aerospace Sciences Meeting and Exhibit Meeting Papers (January, 2005), pp. 11253-11274, Reno, NV, United States [doi]  [abs]
  77. Ekici, K; Voytovycht, DM; Hall, KC, Time-linearized Navier-Stokes analysis of flutter in multistage turbomachines, 43rd Aiaa Aerospace Sciences Meeting and Exhibit Meeting Papers (January, 2005), pp. 14259-14277, Reno, NV, United States [doi]  [abs]
  78. 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]
  79. 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]
  80. Hall, KC; Ekici, K, Multistage coupling for unsteady flows in turbomachinery, Aiaa J. (Usa), vol. 43 no. 3 (2005), pp. 624-632, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452, ISBN 1-4020-4267-1 [Gateway.cgi], [doi]  [abs]
  81. 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]
  82. 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]
  83. 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]
  84. 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]
  85. 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]
  86. 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]
  87. 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]
  88. Hall, KC; Thomas, JP; Ekici, K; Voytovych, DM, Frequency domain techniques for complex and nonlinear flows in turbomachinery, 33rd Aiaa Fluid Dynamics Conference and Exhibit (December, 2003), ISBN 9781624100956  [abs]
  89. 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]
  90. 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]
  91. 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]
  92. 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]
  93. 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]
  94. 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]
  95. Kielb Robert, E; Thomas Jeffrey, P; Barter John, W; Hall Kenneth, C, Blade excitation by aerodynamic instabilities - A compressor blade study, American Society of Mechanical Engineers, International Gas Turbine Institute, Turbo Expo (Publication) Igti, vol. 4 (2003), pp. 399-406, ASME, Atlanta, GA, United States, ISBN 0791836878 [doi]  [abs]
  96. 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]
  97. 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]
  98. Hall, KC; Hall, SR, A rational engineering analysis of the efficiency of flapping flight, edited by Mueller, TJ, Fixed and Flapping Wing Aerodynamics for Micro Air Vehicle Applications, vol. 195 (January, 2002), pp. 249-274, AMER INST AERONAUTICS & ASTRONAUTICS, ISSN 0079-6050, ISBN 1-56347-517-0 [Gateway.cgi]
  99. 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]
  100. 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]
  101. 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]
  102. Hall Kenneth, C; Thomas Jeffrey, P; Clark, WS, Computation of unsteady nonlinear flows in cascades using a harmonic balance technique, Aiaa Journal, vol. 40 no. 5 (2002), pp. 879-886, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  103. 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]
  104. 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]
  105. 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]
  106. Dowell, EH; Thomas, JP; Hall, KC, Transonic limit cycle oscillation analysis using reduced order aerodynamic models, 19th Aiaa Applied Aerodynamics Conference (December, 2001)  [abs]
  107. 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]
  108. 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]
  109. 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]
  110. 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]
  111. 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]
  112. 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]
  113. 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]
  114. 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]
  115. Florea, R; Hall, KC, Sensitivity analysis of unsteady inviscid flow through turbomachinery cascades, Aiaa Journal, vol. 39 no. 6 (January, 2001), pp. 1047-1056 [doi]  [abs]
  116. 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]
  117. Florea, R; Hall, KC, Sensitivity analysis of unsteady inviscid flow through turbomachinery cascades, 38th Aerospace Sciences Meeting and Exhibit, vol. 39 no. 6 (December, 2000), pp. 1047-1056, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
  118. Florea, R; Hall, KC, Sensitivity analysis of unsteady inviscid flow through turbomachinery cascades, 38th Aerospace Sciences Meeting and Exhibit (January, 2000) [doi]  [abs]
  119. 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]
  120. 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]
  121. Clark William, S; Hall Kenneth, C, Time-linearized Navier-Stokes analysis of stall flutter, Journal of Turbomachinery, Transactions of the Asme, vol. 122 no. 3 (2000), pp. 467-476, ASME International [1.1303073], [doi]  [abs]
  122. 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]
  123. Clark, WS; Hall, KC, A time-linearized Navier-Stokes analysis of stall flutter, Proceedings of the Asme Turbo Expo, vol. 4 (January, 1999), ASME, ISBN 9780791878613 [doi]  [abs]
  124. 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]
  125. 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]
  126. 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]
  127. 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), ISBN 9780000000002  [abs]
  128. 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]
  129. 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]
  130. Florea, R; Hall, KC, Eigenmode analysis of unsteady flows about airfoils, Journal of Computational Physics, vol. 147 no. 2 (December, 1998), pp. 568-593, Elsevier BV [doi]  [abs]
  131. Florea, R; Hall, KC; Cizmas, PGA, Eigenmode analysis of unsteady viscous flows in turbomachinery cascades, edited by Fransson, TH, Unsteady Aerodynamics and Aeroelasticity of Turbomachines (January, 1998), pp. 767-782, SPRINGER, ISBN 0-7923-5040-5 [Gateway.cgi]
  132. Florea, R; Hall, KC; Cizmas, PGA, Reduced-order modeling of unsteady viscous flow in a compressor cascade, Aiaa Journal, vol. 36 no. 6 (January, 1998), pp. 1039-1048, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [doi]  [abs]
  133. Hall Kenneth, C; Pigott Steven, A; Hall Steven, R, Power requirements for large-amplitude flapping flight, Journal of Aircraft, vol. 35 no. 3 (1998), pp. 352-361, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0021-8669, ISBN 9780000000002 [doi]  [abs]
  134. Silkowski, PD; Hall, KC, Coupled mode analysis of unsteady multistage flows in turbomachinery, Journal of Turbomachinery, Transactions of the Asme, vol. 120 no. 3 (1998), pp. 410-421, ASME International [doi]  [abs]
  135. Silkowski, PD; Hall, KC, Coupled mode analysis of unsteady multistage flows in turbomachinery, American Society of Mechanical Engineers (Paper) (December, 1997), pp. 15 -, Orlando, FL, USA  [abs]
  136. 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]
  137. Hall, KC; Pigott, SA; Hall, SR, Power requirements for large-amplitude flapping flight, 35th Aerospace Sciences Meeting and Exhibit (January, 1997), pp. 1-11, ISBN 9780000000002  [abs]
  138. Silkowski, PD; Hall, KC, A coupled mode analysis of unsteady multistage flows in turbomachinery, Proceedings of the Asme Turbo Expo, vol. 4 (January, 1997), ASME, ISBN 9780791878712 [doi]  [abs]
  139. Hall, KC; Pigott, SA; Hall, SR, Power requirements for large-amplitude flapping flight, 35th Aerospace Sciences Meeting and Exhibit (January, 1997), pp. 1-11  [abs]
  140. 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]
  141. 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]
  142. Hall, KC; Silkowski, PD, Influence of neighboring blade rows on the unsteady aerodynamic response of cascades, Journal of Turbomachinery, Transactions of the Asme, vol. 119 no. 1 (1997), pp. 85-93, ASME International [doi]  [abs]
  143. Lorence, CB; Hall, KC, Sensitivity analysis of the aeroacoustic response of turbomachinery blade rows, Aiaa Journal, vol. 34 no. 8 (January, 1996), pp. 1545-1554, American Institute of Aeronautics and Astronautics (AIAA), ISBN 9780000000002 [doi]  [abs]
  144. Florea, R; Hall, KC; Cizmas, PGA, Reduced order modelling of unsteady viscous flow in a compressor cascade, 32nd Joint Propulsion Conference and Exhibit (January, 1996), ISBN 9780000000002  [abs]
  145. Florea, R; Hall, KC; Cizmas, PGA, Reduced order modelling of unsteady viscous flow in a compressor cascade, 32nd Joint Propulsion Conference and Exhibit (January, 1996) [doi]  [abs]
  146. Hall Kenneth, C; Hall Steven, R, Minimum induced power requirements for flapping flight, Journal of Fluid Mechanics, vol. 323 no. -1 (1996), pp. 285-315, Cambridge University Press (CUP) [doi]  [abs]
  147. Hall, KC; Florea, R, A reduced order model of unsteady flows in turbomachinery, Journal of Turbomachinery, vol. 117 no. 3 (January, 1995), pp. 375-383, ASME International [doi]  [abs]
  148. Cizmas, PGA; Hall, KC, Computation of steady and unsteady viscous flows using a simultaneously coupled inviscid-viscous interaction technique, Journal of Fluids and Structures, vol. 9 no. 6 (January, 1995), pp. 639-657, Elsevier BV, ISSN 0889-9746 [doi]  [abs]
  149. Hall, KC; Silkowski, PD, Influence of neighboring blade rows on the unsteady aerodynamic response of cascades, American Society of Mechanical Engineers (Paper) (January, 1995), pp. 11pp, Houston, TX, USA  [abs]
  150. Clark, WS; Hall, KC, Numerical model of the onset of stall flutter in cascades, American Society of Mechanical Engineers (Paper) (January, 1995), pp. 11pp, Houston, TX, USA  [abs]
  151. Lorence, CB; Hall, KC, Sensitivity analysis of unsteady aerodynamic loads in cascades, Aiaa Journal, vol. 33 no. 9 (January, 1995), pp. 1604-1610, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  152. Cizmas, PGA; Hall, KC, A viscous-inviscid model of unsteady small-disturbance flows in cascades, 31st Joint Propulsion Conference and Exhibit (January, 1995), ISBN 9780000000002  [abs]
  153. Lorence, CB; Hall, KC, Sensitivity analysis of the aeroacoustic response of turbomachinery blade rows, 33rd Aerospace Sciences Meeting and Exhibit (January, 1995), ISBN 9780000000002 [doi]  [abs]
  154. Clark, WS; Hall, KC, A numerical model of the onset of stall flutter in cascades, Proceedings of the Asme Turbo Expo, vol. 5 (January, 1995), ASME, ISBN 9780791878828 [doi]  [abs]
  155. Hall, KC; Silkowski, PD, The influence of neighboring blade rows on the unsteady aerodynamic response of cascades, Proceedings of the Asme Turbo Expo, vol. 1 (January, 1995), ASME, ISBN 9780791878781 [doi]  [abs]
  156. Lorence, C.B. and Hall, K.C., Sensitivity analysis of unsteady aerodynamic loads in cascades, AIAA Journal, vol. 33 no. 9 (1995), pp. 1604 - 1610  [abs]
  157. Hall, KC, Eigenanalysis of unsteady flows about airfoils, cascades, and wings, Collection of Technical Papers Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference, vol. 2 no. 2 (December, 1994), pp. 967-976, Hilton Head, SC, USA  [abs]
  158. Florea, R; Hall, KC, Reduced order modeling of unsteady flows about airfoils, American Society of Mechanical Engineers, Aerospace Division (Publication) Ad, vol. 44 (December, 1994), pp. 49-68, Chicago, IL, USA  [abs]
  159. Hall, KC; Florea, R; Lanzkron, PJ, Reduced order model of unsteady flows in turbomachinery, American Society of Mechanical Engineers (Paper), vol. 5 (January, 1994), pp. 1-11, ISSN 0402-1215 [doi]  [abs]
  160. Hall, KC; Florea, R; Lanzkron, PJ, A reduced order model of unsteady flows in turbomachinery, Proceedings of the Asme Turbo Expo, vol. 5 (January, 1994), pp. 1-11, ASME, Hague, Neth, ISBN 9780791878873 [doi]  [abs]
  161. Hall, KC, Eigenanalysis of unsteady flows about airfoils, cascades, and wings, Aiaa Journal, vol. 32 no. 12 (January, 1994), pp. 2426-2432, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  162. Hall, SR; Yang, KY; Hall, KC, Helicopter rotor lift distributions for minimum-induced power loss, Journal of Aircraft, vol. 31 no. 4 (January, 1994), pp. 837-845, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  163. Hall, KC; Clark, WS; Lorence, CB, Linearized euler analysis of unsteady transonic flows in turbomachinery, Journal of Turbomachinery, Transactions of the Asme, vol. 116 no. 3 (1994), pp. 477-488, ASME International [doi]  [abs]
  164. Hall, KC; Clark, WS, Errata: Linearized Euler Predictions of Unsteady Aerodynamic Loads in Cascades, Aiaa Journal, vol. 31 no. 5 (May, 1993), pp. 970-970, American Institute of Aeronautics and Astronautics (AIAA), ISSN 0001-1452 [Gateway.cgi], [doi]
  165. Hall, KC; Clark, WS; Lorence, CB, Linearized Euler analysis of unsteady transonic flows in turbomachinery, American Society of Mechanical Engineers (Paper), vol. 1 (January, 1993), ISSN 0402-1215 [doi]  [abs]
  166. Hall, KC; Clark, WS, Linearized euler predictions of unsteady aerodynamic loads in cascades, Aiaa Journal, vol. 31 no. 3 (January, 1993), pp. 540-550, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  167. Hall, KC, Deforming grid variational principle for unsteady small disturbance flows in cascades, Aiaa Journal, vol. 31 no. 5 (January, 1993), pp. 891-900, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  168. Hall, KC; Clark, WS; Lorence, CB, A linearized euler analysis of unsteady transonic flows in turbomachinery, Asme 1993 International Gas Turbine and Aeroengine Congress and Exposition, Gt 1993, vol. 1 (January, 1993), pp. 13 -, Cincinnati, OH, USA, ISBN 9780791878880 [doi]  [abs]
  169. Hall, KC; Lorence, CB, Calculation of three-dimensional unsteady flows in turbomachinery using the linearized harmonic Euler equations, Journal of Turbomachinery, Transactions of the Asme, vol. 115 no. 4 (1993), pp. 800-809, ASME International, ISBN 9780791878972 [doi]  [abs]
  170. Hall, KC; Lorence, CB, Calculation of Three-Dimensional Unsteady Flows in Turbomachinery Using the Linearized Harmonic Euler Equations, Asme 1992 International Gas Turbine and Aeroengine Congress and Exposition, Gt 1992, vol. 5 (January, 1992), ISBN 9780791878972 [doi]  [abs]
  171. Hall, KC; Verdon, JM, Gust response analysis for cascades operating in nonuniform mean flows, Aiaa Journal, vol. 29 no. 9 (January, 1991), pp. 1463-1471, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  172. Verdon, JM; Barnett, M; Hall, KC; Ayer, TC, Development of unsteady aerodynamic analyses for turbomachinery aeroelastic and aeroacoustic applications no. 4405 (1991), pp. 112
  173. Hall, KC; Crawley, EF, Calculation of unsteady flows in turbomachinery using the linearizedEuler equations, Aiaa Journal, vol. 27 no. 6 (January, 1989), pp. 777-787, American Institute of Aeronautics and Astronautics (AIAA) [doi]  [abs]
  174. Crawley, EF; Hall, KC, Optimization and mechanisms of mistuning in cascades, Journal of Engineering for Gas Turbines and Power, vol. 107 no. 2 (January, 1985), pp. 418-426, ASME International, Amsterdam, Neth [doi]  [abs]
  175. Crawley, E. F. and Hall, K. C., OPTIMIZATION AND MECHANISMS OF MISTUNING IN CASCADES., Journal of Engineering for Gas Turbines and Power, Transactions of the ASME, vol. 107 no. 2 (1985), pp. 418 - 426  [abs]
  176. Crawley, EF; Hall, KC, OPTIMIZATION AND MECHANISMS OF MISTUNING IN CASCADES., American Society of Mechanical Engineers (Paper) (January, 1984)
  177. Crawley, EF; Hall, KC, OPTIMIZATION AND MECHANISMS OF MISTUNING IN CASCADES., American Society of Mechanical Engineers (Paper) (January, 1984)
  178. Hall, KC; Johnson, WM, Accurate centroid tracking, Smart Structures and Materials 2005: Active Materials: Behavior and Mechanics, vol. 363 (August, 1983), pp. 106-113, SPIE, San Diego, CA, USA [doi]  [abs]
  179. Hall, K.C. and Hall, S.R., Minimum induced power requirements for flapping flight, J. Fluid Mech. (UK), vol. 323 (25), pp. 285 - 315  [abs]