Earl H. Dowell

Publications

Papers Published

  1. D. Tang and E. H. Dowell, Flutter/LCO suppression for high-aspect ratio wings, Aeronautical Journal, vol 113 no. 1144 (2009), pp. 409 -- 416 [abs].
  2. J. W. Jaworski and E. H. Dowell, Comparison of Theoretical Structural Models with Experiment for a High-Aspect-Ratio Aeroelastic Wing, Journal Of Aircraft, vol 46 no. 2 (2009), pp. 708 -- 713.
  3. K. Ekici and K. C. Hall and E. H. Dowell, Computationally fast harmonic balance methods for unsteady aerodynamic predictions of helicopter rotors, Journal Of Computational Physics, vol 227 no. 12 (2008), pp. 6206 -- 6225 [abs].
  4. J. W. Jaworski and E. H. Dowell, Free vibration of a cantilevered beam with multiple steps: Comparison of several theoretical methods with experiment, Journal Of Sound And Vibration, vol 312 no. 4-5 (2008), pp. 713 -- 725 [abs].
  5. D. Tang and E. H. Dowell, Theoretical and experimental aeroelastic study for folding wing structures, Journal Of Aircraft, vol 45 no. 4 (2008), pp. 1136 -- 1147 [abs].
  6. P. J. Attar and E. H. Dowell and D. Tang, Delta wing with store limit-cycle-oscillation modeling using a high-fidelity structural model, Journal Of Aircraft, vol 45 no. 3 (2008), pp. 1054 -- 1061 [abs].
  7. J. W. Jaworski and E. H. Dowell, Supersonic indicial lift functions from transform methods, Aiaa Journal, vol 45 no. 8 (2007), pp. 2106 -- 2111.
  8. L. Liu and E. H. Dowell and J. P. Thomas, A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces, Journal Of Fluids And Structures, vol 23 no. 3 (2007), pp. 351 -- 363 [abs].
  9. L. P. Liu and E. H. Dowell and K. C. Hall, A novel harmonic balance analysis for the Van Der Pol oscillator, International Journal Of Non-linear Mechanics, vol 42 no. 1 (2007), pp. 2 -- 12 [abs].
  10. D. Tang and E. H. Dowell, Aerodynamic loading for an airfoil with an oscillating gurney flap, Journal Of Aircraft, vol 44 no. 4 (2007), pp. 1245 -- 1257 [abs].
  11. P. J. Attar and E. H. Dowell and J. R. White and J. P. Thomas, Reduced order nonlinear system identification methodology, Aiaa Journal, vol 44 no. 8 (2006), pp. 1895 -- 1904 [abs].
  12. D. Tang and P. Attar and A. Q. Li and E. H. Dowell, Complex dynamics of a pyranose ring structure molecule attached to an atomic force microscope, Nonlinear Dynamics, vol 45 no. 3-4 (2006), pp. 283 -- 303 [abs].
  13. D. Tang and E. H. Dowell, Experimental and theoretical study of gust response for a wing-store model with freeplay, Journal Of Sound And Vibration, vol 295 no. 3-5 (2006), pp. 659 -- 684 [abs].
  14. D. Tang and P. Attar and E. H. Dowell, Flutter/limit cycle oscillation analysis and experiment for wing-store model, Aiaa Journal, vol 44 no. 7 (2006), pp. 1662 -- 1675 [abs].
  15. L. Liu and J. P. Thomas and E. H. Dowell and P. Attar and K. C. Hall, A comparison of classical and high dimensional harmonic balance approaches for a Duffing oscillator, Journal Of Computational Physics, vol 215 no. 1 (2006), pp. 298 -- 320 [abs].
  16. 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].
  17. 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 [abs].
  18. 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].
  19. 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].
  20. 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].
  21. 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].
  22. 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].
  23. 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].
  24. 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].
  25. 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].
  26. 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].
  27. 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].
  28. D. M. Tang and E. H. Dowell, Aerodynamic flow control of an airfoil with small trailing-edge strips, Journal Of Aircraft, vol 43 no. 6 (2006), pp. 1854 -- 1866 [abs].
  29. D. M. Tang and E. H. Dowell, Flutter and limit-cycle oscillations for a wing-store model with freeplay, Journal Of Aircraft, vol 43 no. 2 (2006), pp. 487 -- 503 [abs].
  30. J. P. Thomas and E. H. Dowell and K. C. Hall, Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, Journal Of Aircraft, vol 43 no. 4 (2006), pp. 865 -- 878 [abs].
  31. P. J. Attar and E. H. Dowell, Stochastic analysis of a nonlinear aeroelastic model using the response surface method, Journal Of Aircraft, vol 43 no. 4 (2006), pp. 1044 -- 1052 [abs].
  32. 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].
  33. 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 [abs].
  34. 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 [abs].
  35. Dowell, Earl H. and Epureanu, Bogdan I., Nonlinear: Introduction, Nonlinear Dynamics, vol 39 no. 1-2 (2005), pp. 1 - [s11071-005-6551-0].
  36. 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 [abs].
  37. 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 [abs].
  38. 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 [abs].
  39. 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 [abs].
  40. 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].
  41. 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].
  42. 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].
  43. 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].
  44. 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].
  45. 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].
  46. 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 [abs].
  47. 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].
  48. 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].
  49. 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].
  50. 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 [abs].
  51. 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].
  52. 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].
  53. 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].
  54. 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].
  55. 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].
  56. 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].
  57. 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].
  58. 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].
  59. 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].
  60. 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].
  61. 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 [abs].
  62. 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 [abs].
  63. 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].
  64. 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 [abs].
  65. 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].
  66. 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].
  67. 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 [abs].
  68. 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 [abs].
  69. 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].
  70. 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].
  71. 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].
  72. 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].
  73. 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].
  74. 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].
  75. 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 [abs].
  76. 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 [abs].
  77. 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].
  78. 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].
  79. 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 [abs].
  80. 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 [abs].
  81. 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 [abs].
  82. 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].
  83. 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].
  84. 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].
  85. 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 [abs].
  86. 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 [abs].
  87. 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 [abs].
  88. 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 [abs].
  89. 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].
  90. 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].
  91. 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].
  92. 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].
  93. 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].
  94. 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].
  95. 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].
  96. 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].
  97. 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].
  98. 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 [abs].
  99. 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].
  100. 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].
  101. 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 [abs].
  102. 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].
  103. 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 [abs].
  104. 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 [abs].
  105. 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 [abs].
  106. 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].
  107. 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 [abs].
  108. 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].
  109. 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].
  110. 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].
  111. 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].
  112. 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].
  113. 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].
  114. 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].
  115. 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].
  116. 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].
  117. 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].
  118. 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].
  119. 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].
  120. 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].
  121. 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 [abs].
  122. 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 [abs].
  123. 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].
  124. 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].
  125. 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].
  126. 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].
  127. 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].
  128. 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].
  129. 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].
  130. 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].
  131. 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].
  132. 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].
  133. 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].
  134. 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].
  135. 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].
  136. 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].
  137. 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].
  138. Dowell, E.H., Eigenmode analysis in unsteady aerodynamics: reduced-order models, AIAA J. (USA), vol 34 no. 8 (1996), pp. 1578 - 83 [abs].
  139. 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].
  140. 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].
  141. 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 [abs].
  142. 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].
  143. 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 [abs].
  144. 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 [abs].
  145. 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].
  146. 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 [abs].
  147. 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].
  148. 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].
  149. 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].
  150. 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 -.
  151. 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].
  152. 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].
  153. 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 [abs].
  154. 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 [abs].
  155. 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 [abs].
  156. 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 [abs].
  157. 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].
  158. 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].
  159. 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 -.
  160. 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].
  161. 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].
  162. Dowell, Earl H., Nonlinear aeroelasticity (1993), pp. 213 -.
  163. 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 [abs].
  164. 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 [abs].
  165. 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 [abs].
  166. 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].
  167. 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].
  168. 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].
  169. 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].
  170. 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].
  171. 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].
  172. 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].
  173. 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].
  174. 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].
  175. 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].
  176. 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].
  177. 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 [abs].
  178. 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].
  179. 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].
  180. Dowell, E.H., A chaotic scenario, J. Sound Vib. (UK), vol 144 no. 1 (1991), pp. 179 - 80 [0022-460X(91)90741-2] [abs].
  181. 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].
  182. Dowell, E., Nonlinear aeroelasticity, Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference (1990), pp. 1497 -.
  183. 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 [abs].
  184. 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 [abs].
  185. 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 -.
  186. 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 [abs].
  187. 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].
  188. 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].
  189. 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].
  190. 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].
  191. 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].
  192. 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].
  193. 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].
  194. Dowell, E., Chaotic oscillations in mechanical systems, Comput. Struct. (UK), vol 30 no. 1-2 (1988), pp. 171 - 84 [0045-7949(88)90225-8] [abs].
  195. 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].
  196. 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 [abs].
  197. 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].
  198. 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].
  199. 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].
  200. 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].
  201. 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].
  202. 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].
  203. 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].
  204. 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].
  205. 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].
  206. 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 [abs].
  207. 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 [abs].
  208. 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].
  209. 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].
  210. 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].
  211. 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].
  212. Dowell, E. H., NONLINEAR AEROELASTICITY: AN OVERVIEW., Proceedings of the U.S. National Congress of Applied Mechanics (1986), pp. 171 - 173 [abs].
  213. 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 [abs].
  214. 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].
  215. 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].
  216. 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].
  217. 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].
  218. 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].
  219. 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].
  220. 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].
  221. 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 - [abs].
  222. 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. - [abs].
  223. 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 - [abs].
  224. 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].
  225. 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. - [abs].
  226. 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 [abs].
  227. 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 - [abs].
  228. 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 - [abs].
  229. 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 - [abs].
  230. , FLUID-STRUCTURE INTERACTION AND AERODYNAMIC DAMPING. (1985), pp. 230 - [abs].
  231. , FLUID-STRUCTURE INTERACTION AND AERODYNAMIC DAMPING. (1985), pp. 230 - [abs].
  232. 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].
  233. Ueda, T. and Dowell, E. H., FLUTTER ANALYSIS USING NONLINEAR AERODYNAMIC FORCES., Journal of Aircraft, vol 21 no. 2 (1984), pp. 101 - 109 [abs].
  234. Dowell, E. H., OBSERVATION AND EVOLUTION OF CHAOS FOR AN AUTONOMOUS SYSTEM., American Society of Mechanical Engineers (Paper) (1984), pp. 10 -.
  235. Dowell, E.H., On asymptotic approximations to beam mode shapes, Trans. ASME, J. Appl. Mech. (USA), vol 51 no. 2 (1984), pp. 439 - [abs].
  236. 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].
  237. 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].
  238. 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].
  239. 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].
  240. 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].
  241. 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 [abs].
  242. Dowell, Earl H., NONLINEAR AEROELASTICITY., Advances in the Astronautical Sciences, vol 50 no. pt 2 (1983), pp. 760 - 799.
  243. Tongue, B. H. and Dowell, E. H., COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., American Society of Mechanical Engineers (Paper) (1983), pp. 6 -.
  244. 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].
  245. 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].
  246. 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].
  247. 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].
  248. 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].
  249. 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].
  250. Chao, C. F. and Dowell, E. H. and Bliss, D. B., MODAL ANALYSIS OF INTERIOR NOISE FIELDS., Semiconductor International (1981), pp. 29 - 56 [abs].
  251. Dowell, Earl H., CONTROL LAWS FOR ADAPTIVE WIND TUNNELS., AIAA Journal, vol 19 no. 11 (1981), pp. 1486 - 1488 [abs].
  252. 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 [abs].
  253. 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].
  254. 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].
  255. 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].
  256. 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].
  257. Dowell, Earl H., SIMPLE METHOD FOR CONVERTING FREQUENCY-DOMAIN AERODYNAMICS TO THE TIME DOMAIN., NASA Technical Memorandum no. 81844 (1980), pp. 39 - [abs].
  258. Dowell, Earl H., MASTER PLAN FOR PREDICTION OF VEHICLE INTERIOR NOISE., AIAA Journal, vol 18 no. 4 (1980), pp. 353 - 366 [abs].
  259. 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].
  260. 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 [abs].
  261. 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].
  262. 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].
  263. 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.
  264. 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].
  265. 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 [abs].
  266. 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].
  267. 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.
  268. 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].
  269. 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].
  270. Dowell, E. H., REVERBERATION TIME, ABSORPTION, AND IMPEDANCE., Journal of the Acoustical Society of America, vol 64 no. 1 (1978), pp. 181 - 191 [abs].
  271. Dowell, E. H., COMPLIANT WALL, SUPERSONIC WIND TUNNEL., Aeronautical Journal, vol 82 no. 814 (1978), pp. 448 - 451 [abs].
  272. Dowell, E.H., Reverberation time, absorption, and impedance, J. Acoust. Soc. Am. (USA), vol 64 no. 1 (1978), pp. 181 - 91 [abs].
  273. 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].
  274. 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].
  275. 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].
  276. 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].
  277. 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].
  278. 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].
  279. 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].
  280. 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].
  281. 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].
  282. 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].
  283. 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].
  284. 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].
  285. 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].
  286. Dowell, E.H., Aeroelasticity of plates and shells (1975), pp. xiii+139 - [abs].
  287. Dowell, E. H., RADIATION FROM PANELS AS A SOURCE OF AIRFRAME NOISE., AIAA Journal, vol 13 no. 11 (1975), pp. 1529 - 1530 [abs].
  288. Dowell, E. H., SIMPLIFIED THEORY OF OSCILLATING AIRFOILS IN TRANSONIC FLOW., Magnetohydrodynamics (English translation of Magnitaya Gidrodinamika) (1975), pp. 655 - 679 [abs].
  289. 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].
  290. 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].
  291. 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].
  292. 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].
  293. 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].
  294. 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 [abs].
  295. 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].
  296. 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].
  297. 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].
  298. Dowell, E.H. and Ventres, C.S., Derivation of aerodynamic kernel functions, AIAA J. (USA), vol 11 no. 11 (1973), pp. 1586 - 8 [abs].
  299. Dowell, E. H. and Ventres, C. S., DERIVATION OF AERODYNAMIC KERNEL FUNCTIONS., AIAA Journal, vol 11 no. 11 (1973), pp. 1586 - 1588 [abs].
  300. 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].
  301. 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].
  302. 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].
  303. 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.
  304. 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.
  305. 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 - [abs].
  306. 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].
  307. 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].
  308. Dowell, E.H., Noise or flutter or both?, J. Sound Vib. (UK), vol 11 no. 2 (1970), pp. 159 - 80 [abs].
  309. Dowell, E.H., Nonlinear flutter of curved plates, AIAA Journal, vol 7 no. 3 (1969), pp. 424 - 431 [abs].
  310. 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].
  311. Dowell, E.H. and Ventres, C.S., Nonlinear flutter of loaded plates, AIAA/ASME Structures, Structural Dynamics and Materials Conference (1968), pp. 11 - [abs].
  312. 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].
  313. Dowell, E.H., Nonlinear oscillations of a fluttering plate. II, AIAA J. (USA), vol 5 no. 10 (1967), pp. 1856 - 62 [abs].
  314. 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].
  315. Dowell, E.H., Nonlinear analysis of flutter of plates and shells, ASME -- Fluid-Solid Interaction (1967), pp. 160 - 186 [abs].
  316. Dowell, E.H., Nonlinear oscillations of fluttering plate -- 2, AIAA Journal, vol 5 no. 10 (1967), pp. 1856 - 1862 [abs].
  317. 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].
  318. Dowell, E.H., Nonlinear oscillations of fluttering plate, AIAA Journal, vol 4 no. 7 (1966), pp. 1267 - 1275 [abs].
  319. Dowell, E.H., Flutter of infinitely long plates and shells -- 1, AIAA Journal, vol 4 no. 8 (1966), pp. 1370 - 1377 [abs].
  320. Dowell, E.H., Flutter of infinitely long plates and shells -- 2, AIAA Journal, vol 4 no. 9 (1966), pp. 1510 - 1518 [abs].
  321. 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].
  322. 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].
  323. Dowell, E., Flutter of multibay panels at high supersonic speeds, AIAA Journal, vol 2 no. 10 (1964), pp. 1805 - 1814 [abs].
  324. 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].
  325. 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].
  326. 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].
  327. 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].
  328. Dowell, E.H., Non-linear theory of unstable plane Poiseuille flow, J. Fluid Mech. (UK), vol 38 (3), pp. 401 - 14 [abs].
  329. 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 (0), pp. 1249 - 57 [abs].
  330. 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 (0), pp. 1209 - 17 [abs].
  331. Dowell, E.H., Free vibrations of a linear structure with arbitrary support conditions, Trans. ASME, E, J. Appl. Mech. (USA), vol 38 no. 3 (0), pp. 595 - 600 [abs].
  332. 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 (0), pp. 727 - 32 [abs].
  333. Pezeshki, C. and Dowell, E.H., On chaos and fractal behavior in a generalized Duffing's system, Physica D (Netherlands), vol 32 no. 2 (0), pp. 194 - 209 [0167-2789(88)90051-6] [abs].
  334. Dowell, E.H. and Tang, D., Nonlinear aeroelasticity and unsteady aerodynamics, AIAA J. (USA), vol 40 no. 9 (0), pp. 1697 - 707 [abs].
  335. 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 (0), pp. 531 - 46 [1.1789969] [abs].
  336. Miyazawa, Y. and Dowell, E.H., Approach to modeling and estimation for uncertain systems, J. Guid. Control Dyn. (USA), vol 12 no. 5 (0), pp. 672 - 80 [abs].
  337. Dowell, E.H., Observation and evolution of chaos for an autonomous system, Trans. ASME, J. Appl. Mech. (USA), vol 51 no. 3 (0), pp. 664 - 73 [abs].
  338. 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 (0), pp. 693 - 7 [abs].
  339. 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 (0), pp. 1931 - 6 [abs].
  340. 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 (0), pp. 595 - 600 [abs].