Earl H. Dowell

Publications

  • Xie, D; Xu, M; Dowell, EH,
    Projection-free proper orthogonal decomposition method for a cantilever plate in supersonic flow
    , Journal of Sound and Vibration, vol 333 no. 23 (2014), pp. 6190-6208 [10.1016/j.jsv.2014.06.039] [abs].
  • Yan, S; Dowell, EH; Lin, B,
    Effects of nonlinear damping suspension on nonperiodic motions of a flexible rotor in journal bearings
    , Nonlinear Dynamics, vol 78 no. 2 (2014), pp. 1435-1450 [10.1007/s11071-014-1526-7] [abs].
  • Gibbs, SC; Fichera, S; Zanotti, A; Ricci, S; Dowell, EH,
    Flow field around the flapping flag
    , Journal of Fluids and Structures, vol 48 (2014), pp. 507-513 [10.1016/j.jfluidstructs.2014.02.011] [abs].
  • Tang, D; Dowell, EH,
    Experimental Aerodynamic Response for an Oscillating Airfoil in Buffeting Flow
    , AIAA Journal: devoted to aerospace research and development, vol 52 no. 6 (2014), pp. 1170-1179 [10.2514/1.J052077] [abs].
  • Eugeni, M; Dowell, EH; Mastroddi, F, Post-buckling longterm dynamics of a forced nonlinear beam: A perturbation approach, Journal of Sound and Vibration, vol 333 no. 9 (2014), pp. 2617-2631 [10.1016/j.jsv.2013.12.026] [abs].
  • Wu, ZY; Dowell, EH; Tang, DM,
    Damping Analysis In Beams Subject To Presliding Friction
    , Mechanics Based Design of Structures and Machines: an international journal, vol 42 no. 2 (2014), pp. 229-243 [10.1080/15397734.2013.875858] [abs].
  • Eugeni, M; Dowell, EH; Mastroddi, F,
    Post-buckling longterm dynamics of a forced nonlinear beam: A perturbation approach
    , Journal of Sound and Vibration, vol 333 no. 9 (2014), pp. 2617-2631 [10.1016/j.jsv.2013.12.026] [abs].
  • Tang, D; Zhao, M; Dowell, EH,
    Inextensible Beam and Plate Theory: Computational Analysis and Comparison With Experiment
    , Journal of Applied Mechanics, vol 81 no. 6 (2014), pp. 061009-061009 [10.1115/1.4026800] [abs].
  • Xie, D; Xu, M; Dowell, EH,
    Proper Orthogonal Decomposition Reduced-Order Model for Nonlinear Aeroelastic Oscillations
    , AIAA Journal: devoted to aerospace research and development, vol 52 no. 2 (2014), pp. 229-241 [10.2514/1.J051989] [abs].
  • Goldman, BD; Dowell, EH; Scott, RC, In-flight aeroelastic stability of the thermal protection system on the NASA HIAD, Part I: Linear theory, 55th AIAA/ASMe/ASCE/AHS/SC Structures, Structural Dynamics, and Materials Conference (2014) [10.2514/6.2014-1520] [abs].
  • Gibbs, SC; Fichera, S; Zanotti, A; Ricci, S; Dowell, EH, Flow field around the flapping flag, Journal of Fluids and Structures, vol 48 (2014), pp. 507-513 [10.1016/j.jfluidstructs.2014.02.011] [abs].
  • Gibbs, SC; Warren, JE; Wilkie, WK; Dowell, EH, Stability of rotorcraft for interplanetary space flight, Annual Forum Proceedings, vol 1 (2014), pp. 471-479 [abs].
  • Thomas, JP; Dowell, EH, Discrete adjoint approach for aeroelastic design optimization, AIAA AVIATION 2014 -15th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conference (2014) [abs].
  • Eftekhari, SA; Bakhtiari-Nejad, F; Dowell, EH, Damage detection of an aeroelastic panel using limit cycle oscillation analysis, International Journal of Non-Linear Mechanics, vol 58 (2014), pp. 99-110 [abs].
  • Tang, D; Dowell, EH, Experimental aeroelastic response for a freeplay control surface in buffeting flow, AIAA Journal: devoted to aerospace research and development, vol 51 no. 12 (2013), pp. 2852-2861 [10.2514/1.J052495] [abs].
  • Dowell, EH; Bliss, DB, New Look at Unsteady Supersonic Potential Flow Aerodynamics and Piston Theory, AIAA Journal: devoted to aerospace research and development, vol 51 no. 9 (2013), pp. 2278-2281 [10.2514/1.J052088] [abs].
  • Balajewicz, MJ; Dowell, EH; Noack, BR, Low-dimensional modelling of high-Reynolds-number shear flows incorporating constraints from the Navier-Stokes equation, Journal of Fluid Mechanics, vol 729 (2013), pp. 285-308 [10.1017/jfm.2013.278] [abs].
  • Nefske, DJ; Sung, SH; Dowell, EH, Comment on "On Dowell's simplification for acoustic cavity-structure interaction and consistent alternatives [J. Acoust. Soc. Am. 127, 22-32 (2010)]", Journal of the Acoustical Society of America, vol 133 no. 3 (2013), pp. 1222-1224 [10.1121/1.4788981] [abs].
  • 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 (2013), pp. 52-67 [10.1080/10618562.2012.742512] [abs].
  • Tang, D; Dowell, EH, Computational/Experimental Aeroelastic Study for a Horizontal-Tail Model with Free Play, AIAA Journal: devoted to aerospace research and development, vol 51 no. 2 (2013), pp. 341-352 [10.2514/1.J051781] [abs].
  • Thomas, JP; Custer, CH; Dowell, EH; Hall, KC; Corre, C, Compact implementation strategy for a harmonic balance method within implicit flow solvers, AIAA Journal: devoted to aerospace research and development, vol 51 no. 6 (2013), pp. 1374-1381 [10.2514/1.J051823] [abs].
  • Grasch, AD; Jaworski, JW; Tang, D; Dowell, EH, Resonant frequency determination of a multistore high-altitude/long- endurance wing, AIAA Journal: devoted to aerospace research and development, vol 51 no. 6 (2013), pp. 1277-1283 [10.2514/1.J051499] [abs].
  • Shen, Y; Liu, L; Dowell, EH, Adaptive fault-tolerant robust control for a linear system with adaptive fault identification, IET Control Theory and Applications, vol 7 no. 2 (2013), pp. 246-252 [10.1049/iet-cta.2012.0696] [abs].
  • Gibbs, SC; Guerrant, DV; Wilkie, WK; Dowell, EH, Rectangular solar sail flutter, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2013) [abs].
  • Wang, I; Gibbs, SC; Dowell, EH, Aeroelastic analysis of a folding wing: Comparison of simple and higher fidelity models for a wide range of fold angles, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2013) [abs].
  • Padmanabhan, MA; Pasiliao, CL; Dowell, EH, An approach to aeroelastic modeling and simulation of limit cycle oscillations of aircraft wings with stores, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2013) [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Discrete adjoint method for nonlinear aeroelastic sensitivities for compressible and viscous flows, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2013) [abs].
  • Goldman, BD; Dowell, EH; Scott, RC, Flutter analysis of the thermal protection layer on the NASA HIAD, AIAA Aerodynamic Decelerator Systems (ADS) Conference 2013 (2013) [10.2514/6.2013-1254] [abs].
  • Wang, I; Gibbs, SC; Dowell, EH, Aeroelastic analysis of a folding wing: Comparison of simple and higher fidelity models for a wide range of fold angles, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2013) [10.2514/6.2013-1635] [abs].
  • Gibbs, SC; Guerrant, DV; Wilkie, WK; Dowell, EH, Rectangular solar sail flutter, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2013) [10.2514/6.2013-1945] [abs].
  • 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 (2013) [10.2514/6.2013-1860] [abs].
  • Padmanabhan, MA; Pasiliao, CL; Dowell, EH, An approach to aeroelastic modeling and simulation of Limit Cycle Oscillations of aircraft wings with stores, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2013) [10.2514/6.2013-1837] [abs].
  • Jaworski, JW; Dowell, EH, Scaling analysis for aeroelastic phenomena using the navier-stokes fluid model, AIAA Journal: devoted to aerospace research and development, vol 50 no. 11 (2012), pp. 2622-2626 [10.2514/1.J051727] [abs].
  • Balajewicz, M; Dowell, EH, Stabilization of projection-based reduced order models of the Navier-Stokes, Nonlinear Dynamics, vol 70 no. 2 (2012), pp. 1619-1632 [10.1007/s11071-012-0561-5] [abs].
  • Liu, L; Shen, Y; Dowell, EH; Zhu, C, A general H fault tolerant control and management for a linear system with actuator faults, Automatica, vol 48 no. 8 (2012), pp. 1676-1682 [10.1016/j.automatica.2012.05.018] [abs].
  • Gibbs, SC; Wang, I; Dowell, E, Theory and experiment for flutter of a rectangular plate with a fixed leading edge in three-dimensional axial flow, Journal of Fluids and Structures, vol 34 (2012), pp. 68-83 [10.1016/j.jfluidstructs.2012.06.009] [abs].
  • Wang, I; Gibbs, SC; Dowell, EH, Aeroelastic model of multisegmented folding wings: Theory and experiment, Journal of Aircraft: devoted to aeronautical science and technology, vol 49 no. 3 (2012), pp. 911-921 [10.2514/1.C031589] [abs].
  • Liu, L; Shen, Y; Dowell, EH, Integrated adaptive fault-tolerant H output feedback control with adaptive fault identification, Journal of Guidance, Control, and Dynamics: devoted to the technology of dynamics and control, vol 35 no. 3 (2012), pp. 881-889 [10.2514/1.55199] [abs].
  • Gibbs, SC; Wang, I; Dowell, E, Theory and experiment for flutter of a rectangular plate with a fixed leading edge in three-dimensional axial flow, Journal of Fluids and Structures (2012) [10.1016/j.jfluidstructs.2012.06.009] [abs].
  • Stanton, SC; Erturk, A; Mann, BP; Dowell, EH; Inman, DJ, Nonlinear nonconservative behavior and modeling of piezoelectric energy harvesters including proof mass effects, Journal of Intelligent Material Systems and Structures, vol 23 no. 2 (2012), pp. 183-199 [10.1177/1045389X11432656] [abs].
  • Eftekhari, SA; Bakhtiari-Nejad, F; Dowell, EH, An investigation on the sensitivity of limit cycle oscillations for detecting damage in an aeroelastic panel, Applied Mechanics and Materials, vol 110-116 (2012), pp. 4424-4432 [10.4028/www.scientific.net/AMM.110-116.4424] [abs].
  • Balajewicz, M; Dowell, E, Reduced-order modeling of flutter and limit-cycle oscillations using the sparse volterra series, Journal of Aircraft: devoted to aeronautical science and technology, vol 49 no. 6 (2012), pp. 1803-1812 [10.2514/1.C031637] [abs].
  • 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 (2012) [10.2514/6.2012-1098] [abs].
  • Gibbs, SC; Wang, I; Bloomhardt, E; Dowell, EH, Aeroelastic behavior of noise-reducing membranes for aircraft lifting surfaces part I: Theory, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2012) [abs].
  • Raveh, DE; Dowell, EH, Aeroelastic responses of spring-suspended airfoil systems in transonic buffeting flows, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2012) [abs].
  • Ni, K; Hu, P; Zhao, H; Dowell, EH, Flutter and lco of an all-movable horizontal tail with freeplay, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2012) [abs].
  • Ni, K; Hu, P; Zhao, H; Dowell, EH, Flutter and LCO of an all-movable horizontal tail with freeplay, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012 (2012) [abs].
  • Gibbs, SC; Wang, I; Bloomhardt, E; Dowell, EH, Aeroelastic behavior of noise-reducing membranes for aircraft lifting surfaces part I: Theory, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012 (2012) [abs].
  • Raveh, DE; Dowell, EH, Aeroelastic responses of spring-suspended airfoil systems in transonic buffeting flows, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012 (2012) [abs].
  • Wang, I; Gibbs, SC; Bloomhardt, EM; Dowell, EH, Aeroelastic behavior of noise-reducing membranes for aircraft lifting surfaces part II: Experimen, 53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference 2012 (2012) [abs].
  • Wang, I; IV, SCG; Dowell, EH, Flutter of rectangular plates in three dimensional incompressible flow with various boundary conditions: Theory and experiment, Proceedings of the ASME Design Engineering Technical Conference, vol 1 no. PARTS A AND B (2012), pp. 51-63 [10.1115/DETC2012-70952] [abs].
  • Dunnmon, JA; Stanton, SC; Mann, BP; Dowell, EH, Power extraction from aeroelastic limit cycle oscillations, Journal of Fluids and Structures, vol 27 no. 8 (2011), pp. 1182-1198 [10.1016/j.jfluidstructs.2011.02.003] [abs].
  • Tang, D; Dowell, EH, Aeroelastic response induced by free play, Part 2: Theoretical/experimental correlation analysis, AIAA Journal: devoted to aerospace research and development, vol 49 no. 11 (2011), pp. 2543-2554 [10.2514/1.56300] [abs].
  • Wang, I; Dowell, EH, Structural Dynamics model of multisegmented folding wings: Theory and experiment, Journal of Aircraft: devoted to aeronautical science and technology, vol 48 no. 6 (2011), pp. 2149-2160 [10.2514/1.C031509] [abs].
  • Tang, D; Dowell, EH, Aeroelastic analysis and experiment for wing/store model with stiction nonlinearity, Journal of Aircraft: devoted to aeronautical science and technology, vol 48 no. 5 (2011), pp. 1512-1530 [10.2514/1.C031151] [abs].
  • Tang, D; Dowell, EH, Aeroelastic response induced by free play, Part 1: Theory, AIAA Journal: devoted to aerospace research and development, vol 49 no. 11 (2011), pp. 2532-2542 [10.2514/1.56298] [abs].
  • Dowell, EH, Can solar sails flutter?, AIAA Journal: devoted to aerospace research and development, vol 49 no. 6 (2011), pp. 1305-1306 [10.2514/1.J050900] [abs].
  • Dunnmon, JA; Stanton, SC; Mann, BP; Dowell, EH, Aeroelastic limit cycles as a small scale energy source, Proceedings of the ASME Design Engineering Technical Conference, vol 4 no. PARTS A AND B (2011), pp. 1181-1190 [10.1115/DETC2011-47002] [abs].
  • Eftekhari, SA; Bakhtiari-Nejad, F; Dowell, EH, Bifurcation boundary analysis as a nonlinear damage detection feature: Does it work?, Journal of Fluids and Structures, vol 27 no. 2 (2011), pp. 297-310 [10.1016/j.jfluidstructs.2010.11.006] [abs].
  • Liu, L; Shen, Y; Zhu, C; Dowell, EH, Online selection of H controllers for a faulty linear system, Proceedings of the IEEE Conference on Decision and Control (2011), pp. 2257-2262 [10.1109/CDC.2011.6160496] [abs].
  • Raveh, DE; Dowell, EH, Frequency lock-in phenomenon for oscillating airfoils in buffeting flows, Journal of Fluids and Structures, vol 27 no. 1 (2011), pp. 89-104 [10.1016/j.jfluidstructs.2010.10.001] [abs].
  • Bloomhardt, EM; Dowell, EH, A study of the aeroelastic behavior of flat plates and membranes with mixed boundary conditions in axial subsonic flow, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2011) [10.2514/6.2011-1995] [abs].
  • Wang, I; Dowell, EH, A structural dynamics model of a multi-segmented folding wing: Theory and experiment, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2011) [10.2514/6.2011-1871] [abs].
  • Thomas, JP; Dowell, EH, Airfoil transonic flow buffet calculations using the OVERFLOW 2 flow solver, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2011) [10.2514/6.2011-2077] [abs].
  • Dowell, EH, Comment on "On Dowell's simplification for acoustic cavity-structure interaction and consistent alternatives" [J. Acoust. Soc. Am. 127, 22-32 (2010)]., Journal of the Acoustical Society of America, vol 128 no. 1 (2010), pp. 1-2 [10.1121/1.3436549] [abs].
  • Tang, D; Grasch, A; Dowell, EH, Gust response for flexibly suspended high-aspect ratio wings, AIAA Journal: devoted to aerospace research and development, vol 48 no. 10 (2010), pp. 2430-2444 [10.2514/1.J050309] [abs].
  • Attar, PJ; Tang, D; Dowell, EH, Nonlinear aeroelastic study for folding wing structures, AIAA Journal: devoted to aerospace research and development, vol 48 no. 10 (2010), pp. 2187-2195 [10.2514/1.44868] [abs].
  • Dowell, EH, Transonic unsteady potential flow: Scaling analysis of linear and nonlinear dynamics, AIAA Journal: devoted to aerospace research and development, vol 48 no. 5 (2010), pp. 1017-1019 [10.2514/1.40426] [abs].
  • Tang, D; Dowell, EH, Aeroelastic airfoil with free play at angle of attack with gust excitation, AIAA Journal: devoted to aerospace research and development, vol 48 no. 2 (2010), pp. 427-442 [10.2514/1.44538] [abs].
  • Hu, P; Ni, K; Qu, K; Xue, L; Zhao, H; Dowell, EH, An efficient POD/ROM based aeroelasticity model, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2010) [abs].
  • Lee, DH; Chen, PC; Tang, D; Dowell, EH, Nonlinear gust response of a control surface with free-play, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2010) [abs].
  • 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 (2010) [abs].
  • Dowell, EH, Some recent advances in nonlinear aeroelasticity: Fluid-structure interaction in the 21 st Century, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference (2010) [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Using automatic differentiation to create a nonlinear reduced-order-model aerodynamic solver, AIAA Journal: devoted to aerospace research and development, vol 48 no. 1 (2010), pp. 19-24 [10.2514/1.36414] [abs].
  • Tang, D; Dowell, EH, Flutter/LCO suppression for high-aspect ratio wings, The Aeronautical Journal, vol 113 no. 1144 (2009), pp. 409-416 [abs].
  • Jaworski, JW; Dowell, EH, Comparison of theoretical structural models with experiment for a high-aspect-ratio aeroelastic wing, Journal of Aircraft: devoted to aeronautical science and technology, vol 46 no. 2 (2009), pp. 708-713 [10.2514/1.39244] [abs].
  • 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: devoted to aeronautical science and technology, vol 46 no. 6 (2009), pp. 2069-2076 [10.2514/1.30703] [abs].
  • Dowell, EH; Thomas, JP; Hall, KC; Jr, CMD, Theoretical predictions of F-16 fighter limit cycle oscillations for flight flutter testing, Journal of Aircraft: devoted to aeronautical science and technology, vol 46 no. 5 (2009), pp. 1667-1672 [10.2514/1.42352] [abs].
  • 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 (2009) [abs].
  • Hu, P; Qu, K; Xue, L; Ni, K; Dowell, E, Efficient aeroelastic model updating in support of flight testing, AIAA Atmospheric Flight Mechanics Conference (2009) [abs].
  • Liu, L; Dowell, EH, High dimensional harmonic balance analysis for dynamic piecewise aeroelastic systerms, ASME International Mechanical Engineering Congress and Exposition, Proceedings, vol 12 (2009), pp. 659-669 [abs].
  • Virgin, LN; Dowell, EH; Flowers, G, Nonlinear Vibration (2008), pp. 255-267 [10.1002/9780470209707.ch18] [abs].
  • Jaworski, JW; Dowell, EH, Free vibration of a cantilevered beam with multiple steps: Comparison of several theoretical methods with experiment, Journal of Sound and Vibration, vol 312 no. 4-5 (2008), pp. 713-725 [10.1016/j.jsv.2007.11.010] [abs].
  • 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 (2008), pp. 6206-6225 [10.1016/j.jcp.2008.02.028] [abs].
  • Tang, D; Dowell, EH, Theoretical and experimental aeroelastic study for folding wing structures, Journal of Aircraft: devoted to aeronautical science and technology, vol 45 no. 4 (2008), pp. 1136-1147 [10.2514/1.32754] [abs].
  • Attar, PJ; Dowell, EH; Tang, D, Delta wing with store limit-cycle-oscillation modeling using a high-fidelity structural model, Journal of Aircraft: devoted to aeronautical science and technology, vol 45 no. 3 (2008), pp. 1054-1061 [10.2514/1.32217] [abs].
  • Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Jr, CMD, A new solution method for unsteady flows around oscillating bluff bodies, Solid Mechanics and its Applications, vol 8 (2008), pp. 37-44 [abs].
  • Liu, L; Kalmár-Nagy, T; Dowell, EH, The high dimensional harmonic balance analysis for second-order delay-differential equations, 2007 Proceedings of the ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, DETC2007, vol 5 PART A (2008), pp. 695-702 [10.1115/DETC2007-34396] [abs].
  • Ekici, K; Hall, KC; Dowell, EH, Computationally fast harmonic balance methods for unsteady aerodynamic predictions of helicopter rotors, 46th AIAA Aerospace Sciences Meeting and Exhibit (2008) [abs].
  • Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Li, A; Jr, CMD, 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 (2008), pp. 4002-4014 [abs].
  • Liu, L; 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 (2007), pp. 2-12 [10.1016/j.ijnonlinmec.2006.09.004] [abs].
  • Jaworski, JW; Dowell, EH, Supersonic indicial lift functions from transform methods, AIAA Journal: devoted to aerospace research and development, vol 45 no. 8 (2007), pp. 2106-2111 [10.2514/1.28144] [abs].
  • Tang, D; Dowell, EH, Aerodynamic loading for an airfoil with an oscillating gurney flap, Journal of Aircraft: devoted to aeronautical science and technology, vol 44 no. 4 (2007), pp. 1245-1257 [10.2514/1.26440] [abs].
  • Liu, L; Dowell, EH; Thomas, JP, A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces, Journal of Fluids and Structures, vol 23 no. 3 (2007), pp. 351-363 [10.1016/j.jfluidstructs.2006.09.005] [abs].
  • Li, A; Dowell, EH, Modal reduction of mathematical models of biological molecules, Journal of Computational Physics, vol 211 no. 1 (2006), pp. 262-288 [10.1016/j.jcp.2005.05.021] [abs].
  • Attar, PJ; Dowell, EH, Erratum: Stochastic analysis of a nonlinear aeroelastic model using the response surface method (Journal of Aircraft (2006) (1044)), Journal of Aircraft: devoted to aeronautical science and technology, vol 43 no. 6 (2006) [10.2514/1.28838] [abs].
  • Attar, PJ; Dowell, EH; White, JR; Thomas, JP, Reduced order nonlinear system identification methodology, AIAA Journal: devoted to aerospace research and development, vol 44 no. 8 (2006), pp. 1895-1904 [10.2514/1.16221] [abs].
  • Tang, D; Dowell, EH, Aerodynamic flow control of an airfoil with small trailing-edge strips, Journal of Aircraft: devoted to aeronautical science and technology, vol 43 no. 6 (2006), pp. 1854-1866 [10.2514/1.18969] [abs].
  • Tang, D; Attar, P; Dowell, EH, Flutter/limit cycle oscillation analysis and experiment for wing-store model, AIAA Journal: devoted to aerospace research and development, vol 44 no. 7 (2006), pp. 1662-1675 [10.2514/1.12634] [abs].
  • Tang, D; Attar, P; Li, A; Dowell, EH, Complex dynamics of a pyranose ring structure molecule attached to an atomic force microscope, Nonlinear Dynamics, vol 45 no. 3-4 (2006), pp. 283-303 [10.1007/s11071-006-0508-9] [abs].
  • Tang, D; Dowell, EH, Flutter and limit-cycle oscillations for a wing-store model with freeplay, Journal of Aircraft: devoted to aeronautical science and technology, vol 43 no. 2 (2006), pp. 487-503 [10.1142/S0218127406014952] [abs].
  • Tang, D; Dowell, EH, Experimental and theoretical study of gust response for a wing-store model with freeplay, Journal of Sound and Vibration, vol 295 no. 3-5 (2006), pp. 659-684 [10.1016/j.jsv.2006.01.024] [abs].
  • Liu, L; Thomas, JP; Dowell, EH; Attar, P; Hall, KC, 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 [10.1016/j.jcp.2005.10.026] [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, Journal of Aircraft: devoted to aeronautical science and technology, vol 43 no. 4 (2006), pp. 865-878 [10.2514/1.12349] [abs].
  • Attar, PJ; Dowell, EH, Stochastic analysis of a nonlinear aeroelastic model using the response surface method, Journal of Aircraft: devoted to aeronautical science and technology, vol 43 no. 4 (2006), pp. 1044-1052 [10.2514/1.17525] [abs].
  • 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 (2006), pp. 4549-4558 [abs].
  • 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 (2006), pp. 2437-2449 [abs].
  • Thomas, JP; Dowell, EH; Hall, KC; Jr, CMD, 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 (2006), pp. 3137-3144 [abs].
  • Dowell, EH; Epureanu, BI,
    Introduction
    , Nonlinear Dynamics, vol 39 no. 1-2 (2005), pp. 1-1 [10.1007/s11071-005-6551-0] [abs].
  • Attar, PJ; Dowell, EH; White, JR, Modeling delta wing limit-cycle oscillations using a high-fidelity structural model, Journal of Aircraft: devoted to aeronautical science and technology, vol 42 no. 5 (2005), pp. 1209-1217 [abs].
  • Epureanu, BI; Yin, SH; Dowell, EH, Enhanced nonlinear dynamics for accurate identification of stiffness loss in a thermo-shielding panel, Nonlinear Dynamics, vol 39 no. 1-2 (2005), pp. 197-211 [10.1007/s11071-005-1926-9] [abs].
  • Kanda, A; Dowell, EH, Worst-case gust-response analysis for typical airfoil section with control surface, Journal of Aircraft: devoted to aeronautical science and technology, vol 42 no. 4 (2005), pp. 956-962 [abs].
  • Liu, L; Dowell, EH, Harmonic balance approach for an airfoil with a freeplay control surface, AIAA Journal: devoted to aerospace research and development, vol 43 no. 4 (2005), pp. 802-815 [abs].
  • Thomas, JP; Hall, KC; Dowell, EH, Discrete adjoint approach for modeling unsteady aerodynamic design sensitivities, AIAA Journal: devoted to aerospace research and development, vol 43 no. 9 (2005), pp. 1931-1936 [abs].
  • Attar, PJ; Dowell, EH, A reduced order system ID approach to the modelling of nonlinear structural behavior in aeroelasticity, Journal of Fluids and Structures, vol 21 no. 5-7 SPEC. ISS. (2005), pp. 531-542 [10.1016/j.jfluidstructs.2005.08.012] [abs].
  • Xie, J; Ding, W; Dowell, EH; Virgin, LN, Hopf-flip bifurcation of high dimensional maps and application to vibro-impact systems, Acta Mechanica Sinica, vol 21 no. 4 (2005), pp. 402-410 [10.1007/s10409-005-0045-7] [abs].
  • Attar, PJ; Dowell, EM, A reduced order system ID approach to the modeling of nonlinear structural behavior in aeroelasticity, Proceedings of the ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference - DETC2005, vol 1 B (2005), pp. 1271-1279 [abs].
  • Amabili, M; Dowell, E; Epureanu, BI, Special issue in honour of Professor Michael P. Païdoussis, Journal of Fluids and Structures, vol 21 no. 5-7 SPEC. ISS. (2005), pp. 441-447 [10.1016/j.jfluidstructs.2005.09.001] [abs].
  • Tang, D; Attar, PJ; Dowell, EH, Experimental/theoretical correlation study of nonlinear aeroelasticity for a wing-store model with freeplay, 3rd M.I.T. Conference on Computational Fluid and Solid Mechanics (2005), pp. 1187-1190 [abs].
  • 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 (2005), pp. 4143-4152 [abs].
  • Li, A; Dowell, EH, Modal reduction of mathematical models of biological molecules, Proceedings of the ASME International Design Engineering Technical Conferences and Computers and Information in Engineering Conference - DETC2005, vol 1 C (2005), pp. 1801-1815 [abs].
  • Attar, PJ; Dowell, EH, A stochastic analysis of the limit cycle behavior of a nonlinear aeroelastic model using the response surface method, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 4 (2005), pp. 2318-2338 [abs].
  • Liu, L; Dowell, EH; Thomas, JP, Higher order harmonic balance analysis for limit cycle oscillations in an airfoil with cubic restoring forces, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (2005), pp. 1467-1476 [abs].
  • Thomas, JP; Dowell, EH; Hall, KC; Jr, CMD, 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].
  • Attar, PJ; Dowell, EH; Tang, D, Modeling the LCO of a delta wing with an external store using a high fidelity structural model, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 2 (2005), pp. 1394-1411 [abs].
  • Dowell, EH; Hall, KC; Thomas, JP; Kielb, RE; Spiker, MA; Jr, CMD, Reduced order unsteady aerodynamic models and aeroelasticity, 12th International Congress on Sound and Vibration 2005, ICSV 2005, vol 1 (2005), pp. 47-64 [abs].
  • Dowell, EH; Clark, R; Cox, D; Jr, HCC; Edwards, JW; Hall, KC; Peters, DA; Scanlan, R; Simiu, E; Sisto, F; Strganac, TW, A modern course in aeroelasticity, Solid Mechanics and Its Applications, vol 116 (2005), pp. 1-766 [abs].
  • Tang, D; Li, A; Attar, P; Dowell, EH, Reduced order dynamic model for polysaccharides molecule attached to an atomic force microscope, Journal of Computational Physics, vol 201 no. 2 (2004), pp. 723-752 [10.1016/j.jcp.2004.06.016] [abs].
  • Kholodar, DB; Dowell, EH; Thomas, JP; Hall, KC, Limit-cycle oscillations of a typical airfoil in transonic flow, Journal of Aircraft: devoted to aeronautical science and technology, vol 41 no. 5 (2004), pp. 1067-1072 [abs].
  • Tang, D; Gavin, HP; Dowell, EH, Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 1: Theory, Journal of Sound and Vibration, vol 269 no. 3-5 (2004), pp. 853-874 [10.1016/S0022-460X(03)00180-9] [abs].
  • Tang, D; Gavin, HP; Dowell, EH, Study of airfoil gust response alleviation using an electro-magnetic dry friction damper. Part 2: Experiment, Journal of Sound and Vibration, vol 269 no. 3-5 (2004), pp. 875-897 [10.1016/S0022-460X(03)00181-0] [abs].
  • Tang, D; Dowell, EH, Reduced order model analysis for two-dimensipnal molecular dynamic chain structure attached to an atomic force microscope, Journal of Dynamic Systems Measurement and Control: Transactions of the ASME, vol 126 no. 3 (2004), pp. 531-546 [10.1115/1.1789969] [abs].
  • Liu, L; Dowell, EH, The secondary bifurcation of an aeroelastic airfoil motion: Effect of high harmonics, Nonlinear Dynamics, vol 37 no. 1 (2004), pp. 31-49 [10.1023/B:NODY.0000040033.85421.4d] [abs].
  • Tang, DM; Dowell, EH, Effects of geometric structural nonlinearity of flutter and limit cycle oscillations of high-aspect-ratio wings, Journal of Fluids and Structures, vol 19 no. 3 (2004), pp. 291-306 [10.1016/j.jfluidstructs.2003.10.007] [abs].
  • Tang, D; Dowell, EH, Dynamic analysis of a protein-ligand molecular chain attached to an atomic force microscope, Journal of Vibration and Acoustics: Transactions of the ASME, vol 126 no. 4 (2004), pp. 496-513 [10.1115/1.1804999] [abs].
  • Dowell, EH; Thomas, JP; Hall, KC, Transonic limit cycle oscillation analysis using reduced order aerodynamic models, Journal of Fluids and Structures, vol 19 no. 1 (2004), pp. 17-27 [10.1016/j.jfluidstructs.2003.07.018] [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Modeling viscous transonic limit-cycle oscillation behavior using a harmonic balance approach, Journal of Aircraft: devoted to aeronautical science and technology, vol 41 no. 6 (2004), pp. 1266-1274 [abs].
  • Li, A; Dowell, EH, Asymptotic modal analysis of dynamical systems: The effect of modal cross-correlation, Journal of Sound and Vibration, vol 276 no. 1-2 (2004), pp. 65-80 [10.1016/j.jsv.2003.07.031] [abs].
  • Tang, D; Li, A; Dowell, EH, Transient response study on rolling effectiveness of multiple control surfaces, Journal of Fluids and Structures, vol 19 no. 5 (2004), pp. 621-634 [10.1016/j.jfluidstructs.2004.01.006] [abs].
  • Kholodar, DB; Dowell, EH; Thomas, JP; Hall, KC, Improved understanding of transonic flutter: A three-parameter flutter surface, Journal of Aircraft: devoted to aeronautical science and technology, vol 41 no. 4 (2004), pp. 911-917 [abs].
  • Dowell, EH; Tang, DM, Nonlinear dynamics of very high dimensional fluid-structural systems, Fluid Mechanics and its Applications, vol 75 (2004), pp. 73-113 [10.1007/978-94-007-0995-9_5] [abs].
  • Attar, PJ; Dowell, EH; White, JR, Modeling the LCO of a delta wing using a high fidelity structural model, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (2004), pp. 1986-2000 [abs].
  • Thomas, JP; Dowell, EH; Hall, KC; Jr, CMD, 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].
  • Thomas, JP; Hall, KC; Dowell, EH, A discrete adjoint approach for modeling unsteady aerodynamic design sensitivities, 41st Aerospace Sciences Meeting and Exhibit (2003) [abs].
  • 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 (2003) [abs].
  • 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 (2003) [abs].
  • Tang, D; Gavin, HP; Dowell, EH, Gust alleviation using an electro-magnetic dry friction damper, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2003) [abs].
  • Attar, PJ; Dowell, EH; Tang, D, Modeling aerodynamic nonlinearities for two aeroelastic configurations: Delta wing and flapping flag, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2003) [abs].
  • Dowell, E; Edwards, J; Strganac, TW, Nonlinear aeroelasticity, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference (2003) [abs].
  • Wilson, TL; Dowell, E, Today's ephemera, tomorrow's historical documentation: access options for artists files, J. Libr. Adm. (USA), vol 39 no. 2-3 (2003), pp. 43-60 [10.1300/J111v39n02_05] [abs].
  • Tang, DM; Yamamoto, H; Dowell, EH, Flutter and limit cycle oscillations of two-dimensional panels in three-dimensional axial flow, Journal of Fluids and Structures, vol 17 no. 2 (2003), pp. 225-242 [10.1016/S0889-9746(02)00121-4] [abs].
  • Attar, PJ; Dowell, EH; Tang, DM, A theoretical and experimental investigation of the effects of a steady angle of attack on the nonlinear flutter of a delta wing plate model, Journal of Fluids and Structures, vol 17 no. 2 (2003), pp. 243-259 [10.1016/S0889-9746(02)00123-8] [abs].
  • Epureanu, BI; Dowell, EH, Compact methodology for computing limit-cycle oscillations in aeroelasticity, Journal of Aircraft, vol 40 no. 5 (2003), pp. 955-963 [abs].
  • Dowell, EH; Tang, D, Multiscale, multiphenomena modeling and simulation at the nanoscale: On constructing reduced-order models for nonlinear dynamical systems with many degrees-of-freedom, Journal of Applied Mechanics, Transactions ASME, vol 70 no. 3 (2003), pp. 328-338 [10.1115/1.1558079] [abs].
  • Kholodar, DB; Thomas, JP; Dowell, EH; Hall, KC, Parametric study of flutter for an airfoil in inviscid transonic flow, Journal of Aircraft, vol 40 no. 2 (2003), pp. 303-313 [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Three-dimensional transonic aeroelasticity using proper orthogonal decomposition-based reduced-order models, Journal of Aircraft, vol 40 no. 3 (2003), pp. 544-551 [abs].
  • Epureanu, BI; Dowell, EH, Localized basis function method for computing limit cycle oscillations, Nonlinear Dynamics, vol 31 no. 2 (2003), pp. 151-166 [10.1023/A:1022081101766] [abs].
  • Tang, D; Dowell, EH, Reduced Order Model Analysis For Two Dimensional Molecular Dynamic Chain Structure Attached To An Atomic Force Microscope, American Society of Mechanical Engineers, Design Engineering Division (Publication) DE, vol 116 no. 2 (2003), pp. 905-924 [10.1115/IMECE2003-42496] [abs].
  • Tang, D; Li, A; Dowell, EH, Experimental and theoretical study on rolling effectiveness of multiple control surfaces, AIAA Journal, vol 41 no. 2 (2003), pp. 160-167 [abs].
  • Dowell, EH; Bliss, DB; Clark, RL, Aeroelastic wing with leading- and trailing-edge control surfaces, Journal of Aircraft, vol 40 no. 3 (2003), pp. 559-565 [abs].
  • Dowell, E; Edwards, J; Strganac, T, Nonlinear aeroelasticity, Journal of Aircraft, vol 40 no. 5 (2003), pp. 857-874 [abs].
  • Tang, D; Gavin, HP; Dowell, EH, Theoretical/experimental study of gust alleviation using an electro-magnetic dry friction damper, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 2 (2003), pp. 1092-1108 [abs].
  • 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 (2003), pp. 289-297 [abs].
  • Dowell, E; Edwards, J; Strganac, TW, Nonlinear aeroelasticity, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 5 (2003), pp. 3824-3847 [abs].
  • Attar, PJ; Dowell, EH; Tang, D, Modeling aerodynamic nonlinearities for two aeroelastic configurations: Delta wing and flapping flag, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 1 (2003), pp. 12-22 [abs].
  • 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 (2003), pp. 4779-4784 [abs].
  • Dowell, EH; Tang, D, Nonlinear aeroelasticity and unsteady aerodynamics, 40th AIAA Aerospace Sciences Meeting and Exhibit (2002) [abs].
  • Tang, D; Dowell, EH, Limit cycle oscillations of two-dimensional panels in low subsonic flow, International Journal of Non-Linear Mechanics, vol 37 no. 7 (2002), pp. 1199-1209 [10.1016/S0020-7462(01)00140-8] [abs].
  • Epureanu, BI; Dowell, EH; Hall, KC, Mach number influence on reduced-order models of inviscid potential flows in turbomachinery, Journal of Fluids Engineering, vol 124 no. 4 (2002), pp. 977-987 [10.1115/1.1511165] [abs].
  • 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 (2002), pp. 1323-1334 [10.1115/IMECE2002-32532] [abs].
  • Dowell, EH; Tang, D, Nonlinear aeroelasticity and unsteady aerodynamics, AIAA Journal, vol 40 no. 9 (2002), pp. 1697-1707 [abs].
  • Reichert, WM; Daniels-Race, T; Dowell, EH, Time-tested survival skills for a publish or perish environment, Journal of Engineering Education, vol 91 no. 1 (2002), pp. 133-137 [abs].
  • Tang, D; Dowell, EH, Limit-cycle hysteresis response for a high-aspect-ratio wing model, Journal of Aircraft, vol 39 no. 5 (2002), pp. 885-888 [abs].
  • Juang, JN; Kholodar, D; Dowell, EH, System identification of a vortex lattice aerodynamic model, AIAA Journal, vol 40 no. 6 (2002), pp. 1187-1196 [abs].
  • Tang, D; Li, A; Dowell, EH, Transient response study on rolling effectiveness of multiple control surfaces, ASME International Mechanical Engineering Congress and Exposition, Proceedings (2002), pp. 89-100 [10.1115/IMECE2002-33020] [abs].
  • Tang, D; Dowell, EH, Experimental and theoretical study of gust response for high-aspect-ratio wing, AIAA Journal, vol 40 no. 3 (2002), pp. 419-429 [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Nonlinear inviscid aerodynamic effects on transonic divergence, flutter, and limit-cycle oscillations, AIAA Journal, vol 40 no. 4 (2002), pp. 638-646 [abs].
  • Trickley, ST; Virgin, LN; Dowell, EH, The stability of limit-cycle oscillations in a nonlinear aeroelastic system, Proceedings of the Royal Society of London: Mathematical, Physical and Engineering Sciences, vol 458 no. 2025 (2002), pp. 2203-2226 [10.1098/rspa.2002.0965] [abs].
  • Tang, D; Li, A; Dowell, EH, Transient response study on rolling effectiveness of multiple control surfaces, AMD (Symposia Series) (American Society of Mechanical Engineers, Applied Mechanics Division), vol 253 no. 1 (2002), pp. 89-100 [10.1115/IMECE2002-33020] [abs].
  • Tang, DM; Henry, JK; Dowell, EH, Effects of steady angle of attack on nonlinear gust response of a delta wing model, Journal of Fluids and Structures, vol 16 no. 8 (2002), pp. 1093-1110 [10.1006/jfls.2002.0465] [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, A harmonic balance approach for modeling three-dimensional nonlinear unsteady aerodynamics and aeroelasticity, AMD (Symposia Series) (American Society of Mechanical Engineers, Applied Mechanics Division), vol 253 no. 2 (2002), pp. 1323-1334 [10.1115/IMECE2002-32532] [abs].
  • 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 (2002), pp. 1658-1666 [abs].
  • 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 (2002), pp. 64-79 [abs].
  • Dowell, EH; Thomas, JP; Hall, KC, Transonic limit cycle oscillation analysis using reduced order aerodynamic models, 19th AIAA Applied Aerodynamics Conference (2001) [abs].
  • Heeg, J; Dowell, EH, Characterizing aeroelastic systems using eigenanalysis, explicitly retaining the aerodynamic degrees of freedom, 19th AIAA Applied Aerodynamics Conference (2001) [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Three-Dimensional transonic Aeroelasticity using proper orthogonal decomposition based reduced order models, 19th AIAA Applied Aerodynamics Conference (2001) [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, Nonlinear inviscid aerodynamic effects on transonic divergence, flutter and limit cycle oscillations, 19th AIAA Applied Aerodynamics Conference (2001) [abs].
  • Thomas, JP; Dowell, EH; Hall, KC, A static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics, 39th Aerospace Sciences Meeting and Exhibit (2001) [abs].
  • 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 (2001) [10.1115/2001-GT-0434] [abs].
  • Dowell, EH; Tang, D, Mathematical model of a nanopaddle oscillator, Journal of Applied Physics, vol 90 no. 11 (2001), pp. 5606-5611 [10.1063/1.1415535] [abs].
  • Tang, D; Kholodar, D; Juang, JN; Dowell, EH, System identification and proper orthogonal decomposition method applied to unsteady aerodynamics, AIAA Journal, vol 39 no. 8 (2001), pp. 1569-1576 [abs].
  • Tang, D; Dowell, EH, Experimental and theoretical study on aeroelastic response of high-aspect-ratio wings, AIAA Journal, vol 39 no. 8 (2001), pp. 1430-1441 [abs].
  • Dowell, EH; Hall, KC, Modeling of fluid-structure interaction, Annual Review of Fluid Mechanics, vol 33 (2001), pp. 445-490 [abs].
  • Tang, D; Dowell, EH, Effects of angle of attack on nonlinear flutter of a delta wing, AIAA journal, vol 39 no. 1 (2001), pp. 15-21 [abs].
  • 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 (2001), pp. 2555-2564 [abs].
  • 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 (2001), pp. 255-263 [abs].
  • 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 (2001), pp. 255-273 [10.1006/jfls.2000.0334] [abs].
  • 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 (2001), pp. 230-241 [abs].
  • Trickey, ST; Virgin, LN; Dowell, EH, Characterizing stability of responses in a nonlinear aeroelastic system, 41st Structures, Structural Dynamics, and Materials Conference and Exhibit (2000) [abs].
  • Tang, D; Kholodar, D; Dowell, EH, Nonlinear aeroelastic response of a typical airfoil section with control surface freeplay, 41st Structures, Structural Dynamics, and Materials Conference and Exhibit (2000) [abs].
  • Kholodar, DB; Dowell, EH, The Influence of a Nonzero Angle of Attack and Gust Loads on the Nonlinear Response of a Typical Airfoil Section with a Control Surface Freeplay, International Journal of Nonlinear Sciences and Numerical Simulation, vol 1 no. 3 (2000), pp. 153-165 [abs].
  • Tang, D; Henry, JK; Dowell, EH, Nonlinear aeroelastic response of delta wing to periodic gust, Journal of Aircraft, vol 37 no. 1 (2000), pp. 155-164 [abs].
  • Epureanu, BI; Dowell, EH, Optimal multi-dimensional OGY controller, Physica D: Nonlinear Phenomena, vol 139 no. 1-2 (2000), pp. 87-96 [abs].
  • 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 [abs].
  • Hall, KC; Thomas, JP; Dowell, EH, Proper orthogonal decomposition technique for transonic unsteady aerodynamic flows, AIAA journal, vol 38 no. 10 (2000), pp. 1853-1862 [abs].
  • 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 [10.1006/jfls.2000.0320] [abs].
  • Tang, D; Dowell, EH, Effects of steady angle of attack on nonlinear flutter of a delta wing plate model, American Society of Mechanical Engineers, Applied Mechanics Division, AMD, vol 238 (2000), pp. 37-42 [abs].
  • Tang, D; Kholodar, D; Dowell, EH, Nonlinear response of airfoil section with control surface freeplay to gust loads, AIAA journal, vol 38 no. 9 (2000), pp. 1543-1557 [abs].
  • Clark, RL; Dowell, EH; Frampton, KD, Control of a three-degree-of-freedom airfoil with limit-cycle behavior, Journal of Aircraft, vol 37 no. 3 (2000), pp. 533-536 [abs].
  • Trickey, ST; Virgin, LN; Dowell, EH, 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].
  • Tang, D; Kholodar, D; Dowell, EH, 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].
  • Tang, DM; Dowell, EH; Hall, KC, Limit cycle oscillations of a cantilevered wing in low subsonic flow, AIAA Journal: devoted to aerospace research and development, vol 37 no. 3 (1999), pp. 364-371 [10.2514/2.717] [abs].
  • Epureanu, BI; Dowell, EH; Hall, KC, 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].
  • Finnveden, S; Dowell, EH; Tang, D, Comments on “The high-frequency response of a plate carrying a concentrated mass/spring system” [and reply], J. Sound Vib. (UK), vol 225 no. 4 (1999), pp. 783-800 [10.1006/jsvi.1999.2216] [abs].
  • Tang, D; Henry, JK; Dowell, EH, Limit cycle oscillations of delta wing models in low subsonic flow, AIAA journal, vol 37 no. 11 (1999), pp. 1355-1362 [abs].
  • Kholodar, DB; Dowell, EH, Behavior of airfoil with control surface freeplay for nonzero angles of attack, AIAA journal, vol 37 no. 5 (1999), pp. 651-653 [abs].
  • Tang, D; Dowell, EH; Hall, KC, Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow, AIAA Journal, vol 37 no. 2-3 (1999), pp. 364-371 [abs].
  • Heeg, J; Dowell, EH, Aerodynamic and aeroelastic insights using eigenanalysis, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (1999), pp. 2242-2252 [abs].
  • Tang, D; Henry, JK; Dowell, EH, Limit cycle oscillations of delta wing models in low subsonic flow, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (1999), pp. 2162-2172 [abs].
  • 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 (1999), pp. 622-637 [abs].
  • Virgin, LN; Todd, MD; Begley, CJ; Trickey, ST; Dowell, EH, Basins of attraction in experimental nonlinear oscillators, International Journal of Bifurcation and Chaos in Applied Sciences and Engineering, vol 8 no. 3 (1998), pp. 521-533 [abs].
  • Hu, H; Dowell, EH; Virgin, LN, Resonances of a Harmonically Forced Duffing Oscillator with Time Delay State Feedback, Nonlinear Dynamics, vol 15 no. 4 (1998), pp. 311-327 [abs].
  • Epureanu, BI; Dowell, EH, On the optimality of the Ott-Grebogi-Yorke control scheme, Physica D: Nonlinear Phenomena, vol 116 no. 1-2 (1998), pp. 1-7 [abs].
  • Tang, D; Dowell, EH; Peters, DA, Reduced order aerodynamic models based upon inflow eigenmodes, Journal of the American Helicopter Society, vol 43 no. 4 (1998), pp. 342-351 [abs].
  • Hu, HY; Dowell, EH; Virgin, LN, Stability estimation of high dimensional vibrating systems under state delay feedback control, Journal of Sound and Vibration, vol 214 no. 3 (1998), pp. 497-511 [abs].
  • Tang, D; Dowell, EH, Unsteady aerodynamic forces and aeroelastic response for external store of an aircraft, Journal of Aircraft, vol 35 no. 5 (1998), pp. 678-687 [abs].
  • Dowell, EH; Tang, D, The high-frequency response of a plate carrying a concentrated mass/spring system, Journal of Sound and Vibration, vol 213 no. 5 (1998), pp. 843-863 [abs].
  • Virgin, LN; Dowell, EH; Conner, MD, On the evolution of deterministic non-periodic behavior of an airfoil, International Journal of Non-Linear Mechanics, vol 34 no. 3 (1998), pp. 499-514 [abs].
  • Tang, D; Dowell, EH; Virgin, LN, Limit cycle behavior of an airfoil with a control surface, Journal of Fluids and Structures, vol 12 no. 7 (1998), pp. 839-858 [abs].
  • Vipperman, JS; Clark, RL; Conner, M; Dowell, EH, Experimental active control of a typical section using a trailing-edge flap, Journal of Aircraft: devoted to aeronautical science and technology, vol 35 no. 2 (1998), pp. 224-229 [abs].
  • Dowell, E, Doubling research means doubling education, Scientist, vol 12 no. 5 (1998) [abs].
  • Tang, D; Conner, MD; Dowell, EH, Reduced-order aerodynamic model and its application to a nonlinear aeroelastic system, Journal of Aircraft, vol 35 no. 2 (1998), pp. 332-338 [abs].
  • Reynolds, RR; Dowell, EH, The transient response of structures using asymptotic modal analysis, Journal of Applied Mechanics, vol 65 no. 1 (1998), pp. 258-265 [abs].
  • Epureanu, BI; Dowell, EH, System identification for the Ott-Grebogi-Yorke controller design, Physical Review E: Statistical, Nonlinear, and Soft Matter Physics, vol 56 no. 5 (1997), pp. 5327-5331 [10.1103/PhysRevE.56.5327] [abs].
  • 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 (1997), pp. 149-163 [abs].
  • Conner, MD; Tang, DM; Dowell, EH; Virgin, LN, Nonlinear behavior of a typical airfoil section with control surface freeplay: A numerical and experimental study, Journal of Fluids and Structures, vol 11 no. 1 (1997), pp. 89-109 [abs].
  • Epureanu, BI; Dowell, EH; Montoya, FM, Pattern formation and linear stability analysis in centreless grinding, Proceedings of the Institution of Mechanical Engineers, Part B: Journal of Engineering Manufacture, vol 211 no. B8 (1997), pp. 619-626 [abs].
  • Tang, D; Dowell, EH, Nonlinear rotor aeroelastic analysis with stall and advanced wake dynamics, Journal of Aircraft: devoted to aeronautical science and technology, vol 34 no. 5 (1997), pp. 679-687 [abs].
  • Dowell, EH; Hall, KC; Romanowski, MC, Eigenmode analysis in unsteady aerodynamics: Reduced order models, Applied Mechanics Reviews, vol 50 no. 6 (1997), pp. 371-385 [abs].
  • Epureanu, BI; Dowell, EH, System identification for the Ott-Grebogi-Yorke controller design, Physical Review E - Statistical Physics, Plasmas, Fluids, and Related Interdisciplinary Topics, vol 56 no. 5 SUPPL. A (1997), pp. 5327-5331 [abs].
  • Vipperman, JS; Clark, RL; Conner, M; Dowell, EH, Investigation of the experimental active control of a typical section airfoil using a trailing edge flap, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 1 (1997), pp. 180-189 [abs].
  • Epureanu, BI; Dowell, EH; Montoya, FM, Pattern formation and linear stability analysis in centreless grinding, Proceedings of the Institution of Mechanical Engineers Part B: Journal of Engineering Manufacture, vol 211 no. 8 (1997), pp. 619-625 [abs].
  • Tang, DM; Dowell, EH, Comments on the ONERA stall aerodynamic model and its impact on aeroelastic stability, Journal of Fluids and Structures, vol 10 no. 4 (1996), pp. 353-366 [10.1006/jfls.1996.0023] [abs].
  • Tang, DM; Dowell, EH, Nonlinear response of a non-rotating rotor blade to a periodic gust, Journal of Fluids and Structures, vol 10 no. 7 (1996), pp. 721-742 [10.1006/jfls.1996.0050] [abs].
  • Dowell, EH, Eigenmode analysis in unsteady aerodynamics: Reduced-order models, AIAA Journal, vol 34 no. 8 (1996), pp. 1578-1583 [abs].
  • Dowell, EH, Comment on energy flow predictions in a structure of rigidly joined beams using receptance theory, Journal of Sound and Vibration, vol 194 no. 3 (1996), pp. 445-447 [10.1006/jsvi.1996.0368] [abs].
  • Cizmaş, PGA; Tang, D; Dowell, EH, Flow about a slotted cylinder-airfoil combination in a wind tunnel, Journal of Aircraft, vol 33 no. 4 (1996), pp. 716-721 [abs].
  • Smelova-Reynolds, T; Dowell, EH, The role of higher modes in the chaotic motion of the buckled beam - I, International Journal of Non-Linear Mechanics, vol 31 no. 6 SPEC. ISS. (1996), pp. 931-939 [10.1016/S0020-7462(96)00114-X] [abs].
  • Tang, DM; Cizmas, PGA; Dowell, EH, Experiments and analysis for a gust generator in a wind tunnel, Journal of Aircraft, vol 33 no. 1 (1996), pp. 139-148 [abs].
  • Tang, D; Dowell, EH, Damping prediction for hingeless rotor aeroelastic stability with experimental correlation, Journal of Aircraft, vol 33 no. 6 (1996), pp. 1071-1078 [abs].
  • Smelova-Reynolds, T; Dowell, EH, The role of higher modes in the chaotic motion of the buckled beam - II, International Journal of Non-Linear Mechanics, vol 31 no. 6 SPEC. ISS. (1996), pp. 941-950 [10.1016/S0020-7462(96)00115-1] [abs].
  • Frampton, KD; Clark, RL; Dowell, EH, State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading, Journal of Aircraft, vol 33 no. 4 (1996), pp. 816-822 [abs].
  • Frampton, KD; Clark, RL; Dowell, EH, Active control of panel flutter with piezoelectric transducers, Journal of Aircraft, vol 33 no. 4 (1996), pp. 768-774 [abs].
  • Conner, MD; Virgin, LN; Dowell, EH, Accurate numerical integration of state-space models for aeroelastic systems with free play, AIAA Journal, vol 34 no. 10 (1996), pp. 2202-2205 [abs].
  • Tang, DM; Ilgamov, MA; Dowell, EH, Buckling and post-buckling behavior of a pipe subjected to internal pressure, Journal of Applied Mechanics, vol 62 no. 3 (1995), pp. 595-600 [10.1115/1.2895987] [abs].
  • Franzoni, LP; Dowell, EH, On the accuracy of modal analysis in reverberant acoustical systems with damping, Journal of the Acoustical Society of America, vol 97 no. 1 (1995), pp. 687-690 [10.1121/1.412291] [abs].
  • Tang, DM; Dowell, EH, Response of a nonrotating rotor blade to lateral turbulence part I: theory, Journal of Aircraft, vol 32 no. 1 (1995), pp. 145-153 [abs].
  • Tang, DM; Dowell, EH, Damping prediction for a stalled rotor in flap-lag with experimental correlation, Journal of the American Helicopter Society, vol 40 no. 4 (1995), pp. 79-89 [abs].
  • Romanowski, MC; Dowell, EH, Aeroelastic analysis of an airfoil using eigenmode based reduced order unsteady aerodynamics, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (1995), pp. 1863-1870 [abs].
  • Epstein, RJ; Srinivasan, R; Dowell, EH, Flutter of an infinitely long panel in a duct, AIAA journal, vol 33 no. 1 (1995), pp. 109-115 [abs].
  • Tang, DM; Dowell, EH, Response of a nonrotating rotor blade to lateral turbulence part II: experiment, Journal of Aircraft, vol 32 no. 1 (1995), pp. 154-160 [abs].
  • Tang, DM; Dowell, EH, Experimental investigation of three-dimensional dynamic stall model oscillating in pitch, Journal of Aircraft, vol 32 no. 5 (1995), pp. 1062-1071 [abs].
  • Tang, DM; Dowell, EH, Damping prediction for stalled rotor flap-lag stability with experimental correlation, Applied Mechanics Reviews, vol 48 no. 11/2 (1995) [abs].
  • Gottwald, JA; Virgin, LN; Dowell, EH, Routes to escape from an energy well, Journal of Sound and Vibration, vol 187 no. 1 (1995), pp. 133-144 [10.1006/jsvi.1995.0506] [abs].
  • Dowell, E, Science community must reexamine its own 'contract with America', Scientist, vol 9 no. 4 (1995) [abs].
  • Frampton, KD; Clark, RL; Dowell, EH, State space modeling for aeroelastic panels subject to linearized potential flow aerodynamic loading, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 2 (1995), pp. 1183-1189 [abs].
  • Frampton, KD; Clark, RL; Dowell, EH, Active control of panel flutter with linearized potential flow aerodynamics, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 4 (1995), pp. 2273-2280 [abs].
  • Dowell, EH, Eigenmode analysis in unsteady aerodynamics: Reduced order models, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 4 (1995), pp. 2545-2557 [abs].
  • KATZ, A; DOWELL, E, FROM SINGLE WELL CHAOS TO CROSS WELL CHAOS - A DETAILED EXPLANATION IN TERMS OF MANIFOLD INTERSECTIONS, International Journal of Bifurcation and Chaos in Applied Sciences and Engineering, vol 4 no. 4 (1994), pp. 933-941 [10.1142/S0218127494000666] [abs].
  • Dowell, EH; Murphy, KD; Latz, AL, Simplified predictive criteria for the onset of Chaos, Nonlinear Dynamics, vol 6 no. 3 (1994), pp. 247-263 [abs].
  • Doherty, SM; Dowel, EH, Experimental study of asymptotic modal analysis applied to a rectangular plate with concentrated masses, Journal of Sound and Vibration, vol 170 no. 5 (1994), pp. 671-681 [10.1006/jsvi.1994.1093] [abs].
  • Smelova, TV; Dowell, EH, On necessary conditions for chaotic motion of a buckled plate with external excitation in an aerodynamic flow, American Society of Mechanical Engineers, Applied Mechanics Division, AMD, vol 192 (1994), pp. 327-332 [abs].
  • Romanowski, MC; Dowell, EH, Using eigenmodes to form an efficient Euler based unsteady aerodynamics analysis, American Society of Mechanical Engineers, Aerospace Division (Publication) AD, vol 44 (1994), pp. 147-160 [abs].
  • Ilgamov, MA; Tang, DM; Dowell, EH, Flutter and Forced Response of a Cantilevered Pipe: The Influence of Internal Pressure and Nozzle Discharge, Journal of Fluids and Structures, vol 8 no. 2 (1994), pp. 139-156 [10.1006/jfls.1994.1007] [abs].
  • Hopkins, MA; Dowell, EH, Limited amplitude panel flutter with a temperature differential, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (1994), pp. 1343-1355 [abs].
  • Epstein, RJ; Srinivasan, R; Dowell, EH, Flutter of an infinitely long panel in a duct, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference, vol 3 (1994), pp. 1366-1374 [abs].
  • Lyle, KH; Dowell, EH, Acoustic radiation damping of flat rectangular plates subjected to subsonic flows. Part II: Composite, Journal of Fluids and Structures, vol 8 no. 7 (1994), pp. 737-746 [abs].
  • Lyle, KH; Dowell, EH, Acoustic radiation damping of flat rectangular plates subjected to subsonic flows. Part I: Isotropic, Journal of Fluids and Structures, vol 8 no. 7 (1994), pp. 711-735 [abs].
  • Ilgamov, MA; Tang, DM; Dowell, EH, Flutter and forced response of a cantilevered pipe: the influence of internal pressure and nozzle discharge, Journal of Membrane Science, vol 86 no. 1-2 (1994), pp. 139-156 [abs].
  • Tang, DM; Dowell, EH, Comparison of theory and experiment for non-linear flutter and stall response of a helicopter blade, Journal of Sound and Vibration, vol 165 no. 2 (1993), pp. 251-276 [10.1006/jsvi.1993.1256] [abs].
  • Reynolds, RR; Dowell, EH; Tang, D; Virgin, LN, Nonlinear behavior of low aspect ratio panels in subsonic flow: a preliminary study, American Society of Mechanical Engineers, Aerospace Division (Publication) AD, vol 33 (1993), pp. 9-12 [abs].
  • Tang, DM; Dowell, EH, Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade, AIAA journal, vol 31 no. 6 (1993), pp. 1133-1142 [abs].
  • Reynolds, RR; Virgin, LN; Dowell, EH, High-dimensional chaos cab lead to weak turbulence, Nonlinear Dynamics, vol 4 no. 6 (1993), pp. 531-546 [abs].
  • Tang, DM; Dowell, EH, Nonlinear aeroelasticity in rotorcraft, Mathematical and Computer Modelling, vol 18 no. 3-4 (1993), pp. 157-184 [abs].
  • Mahajan, AJ; Kaza, KRV; Dowell, EH, Semi-Empirical Model for Prediction of Unsteady Forces on an Airfoil with Application to Flutter, Journal of Fluids and Structures, vol 7 no. 1 (1993), pp. 87-103 [10.1006/jfls.1993.1007] [abs].
  • Reynolds, RR; Dowell, EH, 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].
  • Mahajan, AJ; Bakhle, MA; Dowell, EH, Efficient procedure for cascade aeroelastic stability determination using nonlinear, time-marching aerodynamic solvers, Collection of Technical Papers - AIAA/ASME Structures, Structural Dynamics and Materials Conference no. pt 5 (1993), pp. 2856-2866 [abs].
  • PERETTI, L; DOWELL, E, EXPERIMENTAL-VERIFICATION OF THE ASYMPTOTIC MODAL-ANALYSIS METHOD AS APPLIED TO A RECTANGULAR ACOUSTIC CAVITY EXCITED BY STRUCTURAL VIBRATION, Journal of Vibration and Acoustics: Transactions of the ASME, vol 114 no. 4 (1992), pp. 546-554 [10.1115/1.2930297] [abs].
  • KUBOTA, Y; DOWELL, E, ASYMPTOTIC MODAL-ANALYSIS FOR SOUND FIELDS OF A REVERBERANT CHAMBER, Journal of the Acoustical Society of America, vol 92 no. 2 (1992), pp. 1106-1112 [10.1121/1.404038] [abs].
  • Gottwald, JA; Virgin, LN; Dowell, EH, Experimental mimicry of Duffing's equation, Journal of Sound and Vibration, vol 158 no. 3 (1992), pp. 447-467 [abs].
  • Tang, DM; Dowell, EH, Flutter and stall response of a helicopter blade with structural nonlinearity, Journal of Aircraft, vol 29 no. 5 (1992), pp. 953-960 [abs].
  • Peretti, L; Dowell, E, Asymptotic modal analysis of a rectangular acoustic cavity excited by wall vibration, AIAA journal, vol 30 no. 5 (1992), pp. 1191-1198 [abs].
  • Higuchi, K; Dowell, EH, Effect of structural damping on flutter of plates with a follower force, AIAA journal, vol 30 no. 3 (1992), pp. 820-825 [abs].
  • Peretti, L; Dowell, E, Study of intensification zones in a rectangular acoustic cavity, AIAA journal, vol 30 no. 5 (1992), pp. 1199-1206 [abs].
  • Tang, DM; Dowell, EH, Chaotic stall response of helicopter rotor in forward flight, Journal of Fluids and Structures, vol 6 no. 3 (1992), pp. 311-335 [abs].
  • Dowell, EH, Author's reply, Journal of Sound and Vibration, vol 152 no. 2 (1992), pp. 373-374 [abs].
  • Dowell, EH, Nonlinear dynamics and chaos in mechanical systems, International Conference on Fuzzy Theory and Technology Proceedings, Abstracts and Summaries (1992) [abs].
  • Kubota, Y; Dowell, EH, Asymptotic modal analysis for sound fields of a reverberant chamber, Journal of the Acoustical Society of America, vol 92 no. 2 I (1992), pp. 1106-1112 [abs].
  • Mahajan, AJ; Dowell, EH; Bliss, DB, Eigenvalue calculation procedure for an Euler/Navier-Stokes solver with application to flows over airfoils, Journal of Computational Physics, vol 97 no. 2 (1991), pp. 398-413 [abs].
  • Dowell, EH, A chaotic scenario, Journal of Sound and Vibration, vol 144 no. 1 (1991), pp. 179-180 [abs].
  • Mahajan, AJ; Dowell, EH; Bliss, DB, Role of artificial viscosity in Euler and Navier-Stokes solvers, AIAA journal, vol 29 no. 4 (1991), pp. 555-559 [abs].
  • Tang, DM; Dowell, EH, Comparison of theory and experiment for nonlinear flutter and stall response of a helicopter blade, Annual Forum Proceedings - American Helicopter Society (1991), pp. 1413-1425 [abs].
  • Higuchi, K; Dowell, EH, Effect of constant transverse force on chaotic oscillations of sinusoidally excited buckled beam, International Journal of Non-Linear Mechanics, vol 26 no. 3-4 (1991), pp. 419-426 [abs].
  • Weiliang, Y; Dowell, E, Limit cycle oscillation of a fluttering cantilever plate, AIAA journal, vol 29 no. 11 (1991), pp. 1929-1936 [abs].
  • Dowell, EH, Some comments on the 1988 Rayleigh medal lecture. (JSV 133(1), 1-27), Journal of Sound and Vibration, vol 144 no. 2 (1991), pp. 355-356 [abs].
  • DOWELL, E; VIRGIN, L, ON SPATIAL CHAOS, ASYMPTOTIC MODAL-ANALYSIS, AND TURBULENCE, Journal of Applied Mechanics, vol 57 no. 4 (1990), pp. 1094-1097 [10.1115/1.2897637] [abs].
  • Dowell, EH; Katz, AL; Goldman, RL, Static subsonic aeroelastic stability of a shell wrapped around a rigid surface, AIAA Journal, vol 28 no. 4 (1990), pp. 732-739 [abs].
  • Kubota, Y; Sekimoto, S; Dowell, EH, The high-frequency response of a plate carrying a concentrated mass, Journal of Sound and Vibration, vol 138 no. 2 (1990), pp. 321-333 [abs].
  • Peretti, LF; Dowell, EH, Experimental verification of the Asymptotic Modal Analysis method as applied to a rectangular acoustic cavity excited by structural vibration, American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) NCA, vol 9 (1990), pp. 1-7 [abs].
  • Higuchi, K; Dowell, EH, Dynamic stability of a rectangular plate with four free edges subjected to a follower force, AIAA Journal, vol 28 no. 7 (1990), pp. 1300-1305 [abs].
  • Higuchi, K; Dowell, EH, Effect of a structural damping on dynamic stability of a free flexible plate subjected to a follower force, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference no. pt 4 (1990), pp. 1965-1971 [abs].
  • Dowell, EH, Nonlinear aeroelasticity, Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference no. pt 3 (1990), pp. 1497-1509 [abs].
  • Higuchi, K; Dowell, EH, Dynamic stability of a completely free plate subjected to a controlled non-conservative follower force, Journal of Sound and Vibration, vol 132 no. 1 (1989), pp. 115-128 [abs].
  • Higuchi, K; Dowell, EH, Effects of the Poisson ratio and negative thrust on the dynamic stability of a free plate subjected to a follower force, Journal of Sound and Vibration, vol 129 no. 2 (1989), pp. 255-269 [abs].
  • Pezeshki, C; Dowell, EH, Generation and analysis of Lyapunov exponents for the buckled beam, International Journal of Non-Linear Mechanics, vol 24 no. 2 (1989), pp. 79-97 [abs].
  • Miyazawa, Y; Dowell, EH, Approach to modeling and estimation for uncertain systems, Journal of Guidance, Control, and Dynamics, vol 12 no. 5 (1989), pp. 672-680 [abs].
  • Dowell, EH; Pezeshki, C, On necessary and sufficient conditions for chaos to occur in Duffing's equation: an Heuristic approach, Journal of Sound and Vibration, vol 121 no. 2 (1988), pp. 195-200 [abs].
  • Tang, DM; Dowell, EH, ON THE THRESHOLD FORCE FOR CHAOTIC MOTIONS FOR A FORCED BUCKLED BEAM., Journal of Applied Mechanics, Transactions ASME, vol 55 no. 1 (1988), pp. 190-196 [abs].
  • Ferri, AA; Dowell, EH, Frequency domain solutions to multi-degree-of-freedom, dry friction damped systems, Journal of Sound and Vibration, vol 124 no. 2 (1988), pp. 207-224 [abs].
  • Pezeshki, C; Dowell, EH, On Chaos and fractal behavior in a generalized duffing's system, Physica D: Nonlinear Phenomena, vol 32 no. 2 (1988), pp. 194-209 [abs].
  • Dowell, E, Chaotic oscillations in mechanical systems, Computers and Structures, vol 30 no. 1-2 (1988), pp. 171-184 [abs].
  • Kubota, Y; Dionne, HD; Dowell, EH, 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].
  • Miyazawa, Y; Dowell, EH, Estimator for uncertain output matrix systems, IEEE Transactions on Automatic Control, vol 33 no. 10 (1988), pp. 967-969 [10.1109/9.7257] [abs].
  • Tang, DM; Dowell, EH, On the threshold force for chaotic motions for a forced buckled beam, American Society of Mechanical Engineers (Paper) (1988), pp. WA/APM7-WA/APM7 [abs].
  • Miyazawa, Y; Dowell, EH, Principal coordinate realization of state estimation and its application to order reduction, Journal of Guidance, Control, and Dynamics, vol 11 no. 3 (1988), pp. 286-288 [abs].
  • Tang, DM; Dowell, EH, Chaotic oscillations of a cantilevered pipe conveying fluid, Journal of Fluids and Structures, vol 2 no. 3 (1988), pp. 263-283 [abs].
  • Dowell, EH, Chaotic oscillations in mechanical systems, Computational Mechanics, vol 3 no. 3 (1988), pp. 199-216 [10.1007/BF00297446] [abs].
  • KUBOTA, Y; DOWELL, E, ASYMPTOTIC MODAL-ANALYSIS FOR DYNAMIC STRESSES OF A PLATE, Journal of the Acoustical Society of America, vol 81 no. 5 (1987), pp. 1267-1272 [10.1121/1.394530] [abs].
  • Pierre, C; Tang, DM; Dowell, EH, LOCALIZED VIBRATIONS OF DISORDERED MULTISPAN BEAMS: THEORY AND EXPERIMENT., AIAA journal, vol 25 no. 9 (1987), pp. 1249-1257 [abs].
  • Tang, DM; Dowell, EH; Albright, JE, DAMPING IN BEAMS WITH MULTIPLE DRY FRICTION SUPPORTS., Journal of Aircraft, vol 24 no. 11 (1987), pp. 820-832 [abs].
  • Pezeshki, C; Dowell, EH, An examination of initial condition maps for the sinusoidally excited buckled beam modeled by the Duffing's equation, Journal of Sound and Vibration, vol 117 no. 2 (1987), pp. 219-232 [abs].
  • Tang, DM; Dowell, EH, EFFECTS OF NONLINEAR DAMPING IN LANDING GEAR ON HELICOPTER LIMIT CYCLE RESPONSE IN GROUND RESONANCE., Journal of the American Helicopter Society, vol 32 no. 1 (1987), pp. 45-53 [abs].
  • Fang, T; Dowell, EH, TRANSIENT MEAN SQUARE RESPONSE OF RANDOMLY DAMPED LINEAR SYSTEMS., Journal of Sound and Vibration, vol 113 no. 1 (1987), pp. 71-79 [abs].
  • Pierre, C; Dowell, EH, Localization of vibrations by structural irregularity, Journal of Sound and Vibration, vol 114 no. 3 (1987), pp. 549-564 [abs].
  • Fang, T; Dowell, EH, Numerical simulations of periodic and chaotic responses in a stable duffing system, International Journal of Non-Linear Mechanics, vol 22 no. 5 (1987), pp. 401-425 [abs].
  • Fang, T; Dowell, EH, Numerical simulations of jump phenomena in stable Duffing systems, International Journal of Non-Linear Mechanics, vol 22 no. 3 (1987), pp. 267-274 [abs].
  • Dowell, EH, 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 [abs].
  • Dowell, EH, CLASSICAL MODAL ANALYSIS, ASYMPTOTIC MODAL ANALYSIS, AND STATISTICAL ENERGY ANALYSIS., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) NCA, vol 3 (1987), pp. 25-26 [abs].
  • Kubota, Y; Dionne, HD; Dowell, EH, ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF AN ACOUSTIC CAVITY., American Society of Mechanical Engineers, Noise Control and Acoustics Division (Publication) NCA, vol 3 (1987), pp. 27-35 [abs].
  • Kubota, Y; Dowell, EH, Experimental investigation of asymptotic modal analysis for a rectangular plate, Journal of Sound and Vibration, vol 106 no. 2 (1986), pp. 203-216 [abs].
  • Tang, DM; Dowell, EH, Damping in beams and plates due to slipping at the support boundaries, part 2: Numerical and experimental study, Journal of Sound and Vibration, vol 108 no. 3 (1986), pp. 509-522 [abs].
  • Dowell, EH, Damping in beams and plates due to slipping at the support boundaries, Journal of Sound and Vibration, vol 105 no. 2 (1986), pp. 243-253 [abs].
  • Tang, DM; Dowell, EH, RANDOM RESPONSE OF BEAMS AND PLATES WITH SLIPPING AT SUPPORT BOUNDARIES., AIAA journal, vol 24 no. 8 (1986), pp. 1354-1361 [abs].
  • Tang, DM; Dowell, EH, RANDOM RESPONSE OF BEAMS AND PLATES WITH SLIPPING AT SUPPORT BOUNDARIES., Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference no. pt 2 (1986), pp. 411-424 [abs].
  • Dowell, EH; Pezeshki, C, ON THE UNDERSTANDING OF CHAOS IN DUFFINGS EQUATION INCLUDING A COMPARISON WITH EXPERIMENT., Journal of Applied Mechanics, Transactions ASME, vol 53 no. 1 (1986), pp. 5-9 [abs].
  • Tang, DM; Dowell, EH, INFLUENCE OF NONLINEAR BLADE DAMPING ON HELICOPTER GROUND RESONANCE INSTABILITY., Journal of Aircraft, vol 23 no. 2 (1986), pp. 104-110 [abs].
  • Dowell, EH, NONLINEAR AEROELASTICITY: AN OVERVIEW., Proceedings of the U.S. National Congress of Applied Mechanics (1986), pp. 171-173 [abs].
  • Pierre, C; Dowell, EH, STUDY OF DYNAMIC INSTABILITY OF PLATES BY AN EXTENDED INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Ferri, AA; Dowell, EH, The behavior of a linear, damped modal system with a non-linear spring-mass-dry friction damper system attached, part II, Journal of Sound and Vibration, vol 101 no. 1 (1985), pp. 55-74 [abs].
  • Dowell, EH; Kubota, Y, ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Pierre, C; Ferri, AA; Dowell, EH, MULTI-HARMONIC ANALYSIS OF DRY FRICTION DAMPED SYSTEMS USING AN INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Dowell, EH, 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].
  • Pierre, C; Dowell, EH, STUDY OF DYNAMIC INSTABILITY OF PLATES BY AN EXTENDED INCREMENTAL HARMONIC BALANCE METHOD., Journal of Applied Mechanics, Transactions ASME, vol 52 no. 3 (1985), pp. 693-697 [abs].
  • Dowell, EH; Kubota, Y, ASYMPTOTIC MODAL ANALYSIS AND STATISTICAL ENERGY ANALYSIS OF DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Dowell, EH; Pezeshki, C, ON THE UNDERSTANDING OF CHAOS IN DUFFINGS EQUATION INCLUDING A COMPARISON WITH EXPERIMENT., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Moon, FC; Dowell, EH, STRUCTURAL DYNAMICS., AMD (Symposia Series) (American Society of Mechanical Engineers, Applied Mechanics Division), vol 70 (1985), pp. 1287-1289 [abs].
  • Dowell, EH; Pezeshki, C, ON THE UNDERSTANDING OF CHAOS IN DUFFINGS EQUATION INCLUDING A COMPARISON WITH EXPERIMENT., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Pierre, C; Ferri, AA; Dowell, EH, MULTI-HARMONIC ANALYSIS OF DRY FRICTION DAMPED SYSTEMS USING AN INCREMENTAL HARMONIC BALANCE METHOD., American Society of Mechanical Engineers (Paper) (1985) [abs].
  • Dowell, EH, The effects of compliant walls on transition and turbulence., IN: SHEAR FLOW - STRUCTURE INTERACTION PHENOMENA, PRESENTED AT ASME WINTER ANNUAL MEETING, (MIAMI BEACH, U.S.A.: NOV. 17-22,, vol 1 ) (1985), pp. 37-52 [abs].
  • Pierre, C; Ferri, AA; Dowell, EH, Multi-harmonic analysis of dry friction damped systems using an incremental harmonic balance method., TRANS. ASME J. APPL. MECH., vol 52 no. 4 , Dec. 1985 (1985), pp. 958-964 [abs].
  • Ueda, T; Dowell, EH, FLUTTER ANALYSIS USING NONLINEAR AERODYNAMIC FORCES., Journal of Aircraft, vol 21 no. 2 (1984), pp. 101-109 [abs].
  • Ueda, T; Dowell, EH, DOUBLET-POINT METHOD FOR SUPERSONIC UNSTEADY LIFTING SURFACES., AIAA journal, vol 22 no. 2 (1984), pp. 179-186 [abs].
  • Dowell, EH, OBSERVATION AND EVOLUTION OF CHAOS FOR AN AUTONOMOUS SYSTEM., American Society of Mechanical Engineers (Paper) (1984) [abs].
  • Dowell, EH, OBSERVATION AND EVOLUTION OF CHAOS FOR AN AUTONOMOUS SYSTEM., Journal of Applied Mechanics, Transactions ASME, vol 51 no. 3 (1984), pp. 664-673 [abs].
  • Dowell, EH, ON ASYMPTOTIC APPROXIMATIONS TO BEAM MODEL SHAPES., Journal of Applied Mechanics, Transactions ASME, vol 51 no. 2 (1984) [abs].
  • Tongue, BH; Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., Journal of Applied Mechanics, Transactions ASME, vol 50 no. 1 (1983), pp. 204-209 [abs].
  • Dowell, EH; Schwartz, HB, Forced response of a cantilever beam with a dry friction damper attached, part II: Experiment, Journal of Sound and Vibration, vol 91 no. 2 (1983), pp. 269-291 [abs].
  • Dowell, EH; Schwartz, HB, Forced response of a cantilever beam with a dry friction damper attached, part I: Theory, Journal of Sound and Vibration, vol 91 no. 2 (1983), pp. 255-267 [abs].
  • Cui, EJ; Dowell, EH, Postbuckling behavior of rectangular orthotropic plates with two free side edges, International Journal of Mechanical Sciences, vol 25 no. 6 (1983), pp. 429-446 [abs].
  • Dowell, EH; Bland, SR; Williams, MH, LINEAR/NONLINEAR BEHAVIOR IN UNSTEADY TRANSONIC AERODYNAMICS., AIAA journal, vol 21 no. 1 (1983), pp. 38-46 [abs].
  • Dowell, EH, NONLINEAR AEROELASTICITY., Advances in the Astronautical Sciences, vol 50 no. pt 2 (1983), pp. 760-799 [abs].
  • Tongue, BH; Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., American Society of Mechanical Engineers (Paper) (1983) [abs].
  • Dowell, EH; Ueda, T; Goorjian, PM, Transient decay times and mean values of unsteady oscillations in transonic flow, AIAA J. (USA), vol 21 no. 12 (1983), pp. 1762-1764 [abs].
  • Tongue, BH; Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR, NONCONSERVATIVE SYSTEMS., American Society of Mechanical Engineers (Paper) (1983) [abs].
  • Dowell, EH, The behavior of a linear, damped modal system with a non-linear spring-mass-dry friction damper system attached, Journal of Sound and Vibration, vol 89 no. 1 (1983), pp. 65-84 [abs].
  • Ueda, T; Dowell, EH, NEW SOLUTION METHOD FOR LIFTING SURFACES IN SUBSONIC FLOW., AIAA journal, vol 20 no. 3 (1982), pp. 348-355 [abs].
  • Dowell, EH, Component mode analysis of a simple non-linear, non-conservative system, Journal of Sound and Vibration, vol 80 no. 2 (1982), pp. 233-246 [abs].
  • Dowell, EH, Flutter of a buckled plate as an example of chaotic motion of a deterministic autonomous system, Journal of Sound and Vibration, vol 85 no. 3 (1982), pp. 333-344 [abs].
  • Dowell, EH, Non-linear oscillator models in bluff body aero-elasticity, Journal of Sound and Vibration, vol 75 no. 2 (1981), pp. 251-264 [abs].
  • Dowell, EH, CRACK EXTENSION IN A DOUBLE CANTILEVERED BEAM MODEL., Journal of Applied Physics, vol 52 no. 8 (1981), pp. 5356-5360 [10.1063/1.329394] [abs].
  • Dowell, EH; Chao, C-F; Bliss, DB, Absorption material mounted on a moving wall-Fluid/wall boundary condition, J. Acoust. Soc. Am. (USA), vol 70 no. 1 (1981), pp. 244-245 [abs].
  • Chao, CF; Dowell, EH; Bliss, DB, MODAL ANALYSIS OF INTERIOR NOISE FIELDS., Semiconductor International (1981), pp. 29-56 [abs].
  • Dowell, EH, CONTROL LAWS FOR ADAPTIVE WIND TUNNELS., AIAA journal, vol 19 no. 11 (1981), pp. 1486-1488 [abs].
  • Dowell, EH; Bland, SR; Williams, MH, LINEAR/NONLINEAR BEHAVIOR IN UNSTEADY TRANSONIC AERODYNAMICS., Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference no. Pt 2, and (1981), pp. 654-670 [abs].
  • Dowell, EH, SIMPLE METHOD FOR CONVERTING FREQUENCY-DOMAIN AERODYNAMICS TO THE TIME DOMAIN., NASA Technical Memorandum (1980) [abs].
  • Dowell, EH, Master plan for prediction of vehicle interior noise, AIAA journal, vol 18 no. 4 (1980), pp. 353-366 [abs].
  • Dowell, EH, INTERIOR NOISE STUDIES FOR SINGLE- AND DOUBLE-WALLED CYLINDRICAL SHELLS., Journal of Aircraft, vol 17 no. 9 (1980), pp. 690-699 [abs].
  • Dowell, EH; Hodges, DH, Comment on `direct solutions for Strum-Liouville systems with discontinuous coefficients' [and reply by D.H. Hodges], AIAA J. (USA), vol 18 no. 6 (1980), pp. 735-736 [abs].
  • Dowell, EH; Chao, CF; Bliss, DB, ACOUSTOELASTICITY: REVIEW AND EXTENSION., Ammonia Plant Safety (and Related Facilities), vol 2 (1980), pp. 377-402 [abs].
  • Dowell, EH, Bounds on modal damping by a component modes method using Lagrange multipliers, Trans. ASME, J. Appl. Mech. (USA), vol 47 no. 1 (1980), pp. 211-213 [abs].
  • Dowell, EH, SIMPLIFIED THEORY OF OSCILLATING AEROFOILS IN TRANSONIC FLOW: REVIEW AND EXTENSION., Aeronautical Quarterly, vol 31 no. pt 4 (1980), pp. 252-284 [abs].
  • Dowell, EH, COMPONENT MODE ANALYSIS OF NONLINEAR AND NONCONSERVATIVE SYSTEMS., Journal of Applied Mechanics, Transactions ASME, vol 47 no. 1 (1980), pp. 172-176 [abs].
  • Horikawa, H; Dowell, EH, An elementary explanation of the flutter mechanism with active feedback controls, J. Aircr. (USA), vol 16 no. 4 (1979), pp. 225-232 [abs].
  • Dowell, EH, ON SOME GENERAL PROPERTIES OF COMBINED DYNAMICAL SYSTEMS., Journal of Applied Mechanics, Transactions ASME, vol 46 no. 1 (1979), pp. 206-209 [abs].
  • Horikawa, H; Dowell, EH, ELEMENTARY EXPLANATION OF THE FLUTTER MECHANISM WITH ACTIVE FEEDBACK CONTROLS., J Aircr, vol 16 no. 4 (1979), pp. 225-232 [abs].
  • Ch'ng, E; Dowell, EH, THEORETICAL ANALYSIS OF NONLINEAR EFFECTS ON THE FLUTTER AND DIVERGENCE OF A TUBE CONVEYING FLUID. (1979), pp. 65-81 [abs].
  • Dowell, EH, Flutter of plates and shells in practice. (1979), pp. Karlsruhe-Sess [abs].
  • Horikawa, H; Dowell, EH; Moon, FC, Active feedback control of a beam subjected to a nonconservative force, International Journal of Solids and Structures, vol 14 no. 10 (1978), pp. 821-839 [abs].
  • Dowell, EH, Reverberation time, absorption, and impedance, Journal of the Acoustical Society of America, vol 64 no. 1 (1978), pp. 181-191 [abs].
  • Dowell, EH, COMPLIANT WALL, SUPERSONIC WIND TUNNEL., Aeronaut J, vol 82 no. 814 (1978), pp. 448-451 [abs].
  • Alexandridis, AA; Dowell, EH; Moon, FC, COUPLED RESPONSE OF A DYNAMIC ELEMENT RIDING ON A CONTINUOUSLY SUPPORTED BEAM., J Appl Mech Trans ASME, vol 45 no. 4 (1978), pp. 864-870 [abs].
  • Dowell, EH, Comments on non-linear flexural vibrations of a cylindrical shell, Journal of Sound and Vibration, vol 60 no. 4 (1978), pp. 596-597 [abs].
  • Dowell, EH, ON SOME GENERAL PROPERTIES OF COMBINED DYNAMICAL SYSTEMS., American Society of Mechanical Engineers (Paper) no. 78 -WA/APM-26 (1978) [abs].
  • Williams, MH; Chi, MR; Ventres, CS; Dowell, EH, AERODYNAMIC EFFECTS OF INVISCID PARALLEL SHEAR FLOWS., AIAA Journal, vol 15 no. 8 (1977), pp. 1159-1166 [abs].
  • Dowell, EH; Traybar, J; Hodges, DH, An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam, Journal of Sound and Vibration, vol 50 no. 4 (1977), pp. 533-544 [abs].
  • Dowell, EH; III, GFG; Smith, DA, Acoustoelasticity: General theory, acoustic natural modes and forced response to sinusoidal excitation, including comparisons with experiment, Journal of Sound and Vibration, vol 52 no. 4 (1977), pp. 519-542 [abs].
  • Dowell, EH; Chi, MR, Variable thickness shear layer aerodynamics revisited, AIAA J. (USA), vol 15 no. 5 (1977), pp. 745-747 [abs].
  • Dowell, EH; Ventres, CS, Flutter of an elastic plate under tension, AIAA J. (USA), vol 15 no. 11 (1977), pp. 1653-1655 [abs].
  • Vaicaitis, R; Dowell, EH, RESPONSE OF SPACE SHUTTLE SURFACE INSULATION PANELS TO ACOUSTIC PRESSURE., Journal of Spacecraft and Rockets, vol 14 no. 12 (1977), pp. 739-746 [abs].
  • Dowell, EH, Comments on "On collapse and flutter phenomena in thin tubes conveying fluid" by D.S. Weaver and M.P. Paidoussis, Journal of Sound and Vibration, vol 55 no. 2 (1977), pp. 312-314 [abs].
  • Dowell, EH; Chi, MR, Variable thickness shear layer aerodynamics revis ited., AIAA Journal, vol 15 no. 5 ,May 1977 (1977), pp. 745-747 [abs].
  • Kornecki, A; Dowell, EH; O'Brien, J, On the aeroelastic instability of two-dimensional panels in uniform incompressible flow, Journal of Sound and Vibration, vol 47 no. 2 (1976), pp. 163-178 [abs].
  • Dowell, EH, VIBRATION AND FLUTTER ANALYSIS OF REUSABLE SURFACE INSULATION PANELS., Journal of Spacecraft and Rockets, vol 12 no. 1 (1975), pp. 44-50 [abs].
  • Dowell, EH, RADIATION FROM PANELS AS A SOURCE OF AIRFRAME NOISE., AIAA Journal, vol 13 no. 11 (1975), pp. 1529-1530 [abs].
  • McLean, JD; Dowell, EH, SWIRLING FLOWS BETWEEN COAXIAL CYLINDERS WITH INJECTION BY RADIAL JETS., AIAA Journal, vol 13 no. 11 (1975), pp. 1435-1440 [abs].
  • Dowell, EH, SIMPLIFIED THEORY OF OSCILLATING AIRFOILS IN TRANSONIC FLOW. (1975), pp. 655-679 [abs].
  • MCLEAN, JD; DOWELL, EH, SWIRLING FLOWS BETWEEN COAXIAL CYLINDERS WITH INJECTION BY RADIAL JETS, A.I.A.A. J. (AM. INST. AERONAUT. ASTRONAUT.), vol 13 no. 10 (1975), pp. NOVEMBER-1975 [abs].
  • DOWELL, EH, AEROELASTICITY OF PLATES AND SHELLS. (1975) [abs].
  • Kalmbach, CF; Dowell, EH; Moon, FC, The suppression of a dynamic instability of an elastic body using feedback control, International Journal of Solids and Structures, vol 10 no. 3 (1974), pp. 361-381 [abs].
  • Vaicaitis, R; Dowell, EH; Ventres, CS, NONLINEAR PANEL RESPONSE BY A MONTE CARLO APPROACH., AIAA Journal, vol 12 no. 5 (1974), pp. 685-691 [abs].
  • Klein, LR; Dowell, EH, 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].
  • Dowell, EH; Srinivasan, AV; McClean, JD; Ambrose, J, AEROELASTIC STABILITY OF CYLINDRICAL SHELLS SUBJECTED TO A ROTATING FLOW., AIAA Journal, vol 12 no. 12 (1974), pp. 1644-1651 [abs].
  • Dowell, EH, Dynamic analysis of an elastic plate on a thin, elastic foundation, Journal of Sound and Vibration, vol 35 no. 3 (1974), pp. 343-360 [abs].
  • Yan, MJ; Dowell, EH, 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].
  • Yan, MJ; Dowell, EH, Elastic sandwich beam or plate equations equivalent to classical theory, Trans. ASME, E, J. Appl. Mech. (USA), vol 41 no. 2 (1974), pp. 526-527 [abs].
  • DOWELL, EH; MCLEAN, JD; AMBROSE, J; SRINIVASAN, AV, AEROELASTIC STABILITY OF CYLINDRICAL SHELLS SUBJECTED TO A ROTATING FLOW., AIAA Journal, vol 12 no. 12 (1974), pp. DECEMBER-1974 [abs].
  • Dowell, EH, Comments on "Vibrations of point supported plates", Journal of Sound and Vibration, vol 32 no. 4 (1974) [abs].
  • Yan, M-J; Dowell, ; H, E, High-damping measurements and a preliminary evaluation of an equation for constrained-layer damping, AIAA J. (USA), vol 11 no. 3 (1973), pp. 388-390 [abs].
  • Dowell, EH; Ventres, CS, DERIVATION OF AERODYNAMIC KERNEL FUNCTIONS., AIAA Journal, vol 11 no. 11 (1973), pp. 1586-1588 [abs].
  • Dowell, EH, THEORETICAL VIBRATION AND FLUTTER STUDIES OF POINT SUPPORTED PANELS., Journal of Spacecraft and Rockets, vol 10 no. 6 (1973), pp. 389-395 [abs].
  • Yan, MJ; Dowell, EH, 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 [abs].
  • Dowell, EH, 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 [abs].
  • Yan, MJ; Dowell, EH, Governing equations for vibrating constrained-layer damping sandwich plates and beams, Trans. ASME, E, J. Appl. Mech. (USA), vol 39 no. 4 (1972), pp. 1041-1046 [abs].
  • DOWELL, E, Free vibrations of a linear structure with arbitrary support conditions, Journal of Applied Mechanics, Transactions ASME, vol 38 Ser E no. 3 (1971), pp. 595-600 [abs].
  • DOWELL, E, COMMENTS ON '%'TURBULENCE-INDUCED PLATE VIBRATIONS. AN EVALUATION OF FINITE-AND INFINITE- PLATE MODELS'%', Journal of the Acoustical Society of America, vol 49 no. 1 pt 2 (1971), pp. 376-379 [abs].
  • DOWELL, E, Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutter, AIAA Journal, vol 9 no. 5 (1971), pp. 834-841 [abs].
  • LAI, J; DOWELL, E; TAUCHERT, T, PROPAGATION OF HARMONIC WAVES IN A COMPOSITE ELASTIC CYLINDER, Journal of the Acoustical Society of America, vol 49 no. 1 pt 2 (1971), pp. 220-228 [abs].
  • Lai, J-L; Dowell, EH; Tauchert, TR, Propagation of harmonic waves in a composite elastic cylinder, J. Acoust. Soc. Am. (USA), vol 49 no. 1 (1971), pp. 220-228 [abs].
  • Dowell, EH, Comments on `turbulence-induced plate vibrations: An evaluation of finite- and infinite-plate models', J. Acoust. Soc. Am. (USA), vol 49 no. 1 (1971) [abs].
  • VENTRES, C; DOWELL, E, COMPARISON OF THEORY AND EXPERIMENT FOR NONLINEAR FLUTTER OF LOADED PLATES, AIAA Journal, vol 8 no. 11 (1970), pp. 2022-2030 [abs].
  • DOWELL, E, FATIGUE LIFE ESTIMATION OF FLUTTERING PANELS, AIAA Journal, vol 8 no. 10 (1970), pp. 1879-1881 [abs].
  • DOWELL, E, FLUTTER OF BUCKLED PLATES AT ZERO DYNAMIC PRESSURE, AIAA Journal, vol 8 no. 3 (1970), pp. 583-584 [abs].
  • DOWELL, E; VENTRES, C, FLUTTER OF LOW ASPECT RATIO PLATES, AIAA Journal, vol 8 no. 6 (1970), pp. 1162-1164 [abs].
  • DOWELL, E, PANEL FLUTTER, A REVIEW OF THE AEROELASTIC STABILITY OF PLATES AND SHELLS, AIAA Journal, vol 8 no. 3 (1970), pp. 385-399 [abs].
  • DOWELL, E, NONLINEAR FLUTTER OF CURVED PLATES, II, AIAA Journal, vol 8 no. 2 (1970), pp. 259-261 [abs].
  • Dowell, EH, Noise or flutter or both?, Journal of Sound and Vibration, vol 11 no. 2 (1970), pp. 159-180 [abs].
  • DOWELL, E, TRANSMISSION OF NOISE FROM A TURBULENT BOUNDARY LAYER THROUGH A FLEXIBLE PLATE INTO A CLOSE CAVITY, Acoustical Soc America-J, vol 46 no. 1 pt 2 (1969), pp. 238-252 [abs].
  • Dowell, EH, Nonlinear flutter of curved plates, AIAA Journal, vol 7 no. 3 (1969), pp. 424-431 [abs].
  • Dowell, EH; Ventres, CS, Modal equations for the nonlinear flexural vibrations of a cylindrical shell, International Journal of Solids and Structures, vol 4 no. 10 (1968), pp. 975-991 [abs].
  • Widnall, SE; Dowell, EH, Aerodynamic forces on an oscillating cylindrical duct with an internal flow, Journal of Sound and Vibration, vol 6 no. 1 (1967), pp. 71-85 [abs].
  • Dowell, EH, Nonlinear analysis of flutter of plates and shells, ASME -- Fluid-Solid Interaction (1967), pp. 160-186 [abs].
  • Dowell, EH, Nonlinear oscillations of a fluttering plate. II, AIAA J. (USA), vol 5 no. 10 (1967), pp. 1856-1862 [abs].
  • Dowell, EH, Generalized aerodynamic forces on flexible plate undergoing transient motion, Quarterly of Applied Mathematics, vol 24 no. 4 (1967), pp. 331-338 [abs].
  • Dowell, EH, Response of plates to fluid loading, Journal of Sound and Vibration, vol 6 no. 1 (1967), pp. 164-165 [abs].
  • Dowell, EH, Nonlinear oscillations of fluttering plate, AIAA Journal, vol 4 no. 7 (1966), pp. 1267-1275 [abs].
  • Dowell, EH, Flutter of infinitely long plates and shells -- 1, AIAA Journal, vol 4 no. 8 (1966), pp. 1370-1377 [abs].
  • Dowell, EH, Flutter of infinitely long plates and shells -- 2, AIAA Journal, vol 4 no. 9 (1966), pp. 1510-1518 [abs].
  • Dowell, EH; Widnall, SE, Generalized aerodynamic forces on oscillating cylindrical shell -- Subsonic and supersonic flow, AIAA Journal, vol 4 no. 4 (1966), pp. 607-610 [abs].
  • Dowell, EH; Voss, HM, Theoretical and experimental panel flutter studies in mach number range 1.0 to 5.0, AIAA Journal, vol 3 no. 12 (1965), pp. 2292-2304 [abs].
  • Dowell, E, Flutter of multibay panels at high supersonic speeds, AIAA Journal, vol 2 no. 10 (1964), pp. 1805-1814 [abs].
  • Dugundji, J; Dowell, E; Perkin, B, Subsonic flutter of panels on continuous elastic foundations, AIAA Journal, vol 1 no. 5 (1963), pp. 1146-1154 [abs].
  • Dowell, EH, Free vibrations of a linear structure with arbitrary support conditions, Trans. ASME, E, J. Appl. Mech. (USA), vol 38 no. 3, pp. 595-600 [abs].
  • Dowell, EH, Free vibrations of an arbitrary structure in terms of component modes, Trans. ASME, E, J. Appl. Mech. (USA), vol 39 no. 3, pp. 727-732 [abs].
  • Dowell, EH, Non-linear theory of unstable plane Poiseuille flow, J. Fluid Mech. (UK), vol 38, pp. 401-414 [abs].
  • Dowell, EH; Williams, MH; Chi, MR, ASSESSMENT OF THEORETICAL MODELS FOR VISCOUS AND TRANSONIC FLOW., AGARD Conference Proceedings [abs].