Year |
Citation |
Score |
2020 |
Ma Z, Lei L, Dowell E, Zeng P. An Experimental Study on the Actuator Line Method with Anisotropic Regularization Kernel Energies. 13: 977. DOI: 10.3390/En13040977 |
0.352 |
|
2020 |
Padmanabhan MA, Dowell EH. Gust Response Computations with Control Surface Freeplay Using Random Input Describing Functions Aiaa Journal. 58: 2899-2908. DOI: 10.2514/1.J059218 |
0.313 |
|
2020 |
Bueno DD, Dowell EH. Revisiting the Fundamentals of Control Surface Reversal Including Nonlinear Effects Journal of Aircraft. 1-8. DOI: 10.2514/1.C035885 |
0.322 |
|
2020 |
Amirzadegan S, Dowell EH. Nonlinear Limit Cycle Oscillation and Flutter Analysis of Clamped Curved Plates Journal of Aircraft. 57: 368-376. DOI: 10.2514/1.C035716 |
0.404 |
|
2020 |
Wayhs-Lopes LD, Dowell EH, Bueno DD. Influence of friction and asymmetric freeplay on the limit cycle oscillation in aeroelastic system: An extended Hénon’s technique to temporal integration Journal of Fluids and Structures. 96: 103054. DOI: 10.1016/J.Jfluidstructs.2020.103054 |
0.425 |
|
2020 |
Modaress-Aval AH, Bakhtiari-Nejad F, Dowell EH, Shahverdi H, Rostami H, Peters D. Aeroelastic analysis of cantilever plates using Peters’ aerodynamic model, and the influence of choosing beam or plate theories as the structural model Journal of Fluids and Structures. 96: 103010. DOI: 10.1016/J.Jfluidstructs.2020.103010 |
0.395 |
|
2020 |
Freydin M, Dowell EH, Whalen TJ, Laurence SJ. A theoretical computational model of a plate in hypersonic flow Journal of Fluids and Structures. 93: 102858. DOI: 10.1016/J.Jfluidstructs.2019.102858 |
0.479 |
|
2020 |
Lee MW, Dowell EH. Improving the predictable accuracy of fluid Galerkin reduced-order models using two POD bases Nonlinear Dynamics. 101: 1-15. DOI: 10.1007/S11071-020-05833-X |
0.428 |
|
2020 |
Freydin M, Dowell EH, Spottswood SM, Perez RA. Nonlinear dynamics and flutter of plate and cavity in response to supersonic wind tunnel start Nonlinear Dynamics. 1-18. DOI: 10.1007/S11071-020-05817-X |
0.343 |
|
2019 |
Amirzadegan S, Dowell EH. Correlation of Experimental and Computational Results for Flutter of Streamwise Curved Plate Aiaa Journal. 57: 3556-3561. DOI: 10.2514/1.J057909 |
0.376 |
|
2019 |
Poplingher L, Raveh DE, Dowell EH. Modal Analysis of Transonic Shock Buffet on 2D Airfoil Aiaa Journal. 57: 2851-2866. DOI: 10.2514/1.J057893 |
0.306 |
|
2019 |
Thomas JP, Dowell EH. Discrete Adjoint Approach for Nonlinear Unsteady Aeroelastic Design Optimization Aiaa Journal. 57: 4368-4376. DOI: 10.2514/1.J057504 |
0.359 |
|
2019 |
Thomas JP, Dowell EH, Anderson M, McGowan GZ. Progress Toward Efficient Compression Algorithms for Application in Flight Simulation Environments Journal of Aerospace Information Systems. 16: 278-288. DOI: 10.2514/1.I010688 |
0.343 |
|
2019 |
Wei Y, Dowell EH, Chen Z. Numerical Prediction of Impact of Clearance on Rotordynamic Coefficients for Labyrinth Brush Seal International Journal of Turbo & Jet-Engines. 36: 31-43. DOI: 10.1515/Tjj-2016-0065 |
0.347 |
|
2019 |
McHugh KA, Dowell EH. Nonlinear Response of an Inextensible, Cantilevered Beam Subjected to a Nonconservative Follower Force Journal of Computational and Nonlinear Dynamics. 14. DOI: 10.1115/1.4042324 |
0.415 |
|
2019 |
Culver D, McHugh K, Dowell E. An assessment and extension of geometrically nonlinear beam theories Mechanical Systems and Signal Processing. 134: 106340. DOI: 10.1016/J.Ymssp.2019.106340 |
0.331 |
|
2019 |
Tang D, Levin D, Dowell E. Experimental and theoretical correlations for energy harvesting from a large flapping flag response Journal of Fluids and Structures. 86: 290-315. DOI: 10.1016/J.Jfluidstructs.2019.02.018 |
0.32 |
|
2019 |
Modaress-Aval AH, Bakhtiari-Nejad F, Dowell EH, Peters DA, Shahverdi H. A comparative study of nonlinear aeroelastic models for high aspect ratio wings Journal of Fluids and Structures. 85: 249-274. DOI: 10.1016/J.Jfluidstructs.2019.01.003 |
0.457 |
|
2019 |
Lee MW, Dowell EH, Balajewicz MJ. A study of the regularized lid-driven cavity’s progression to chaos Communications in Nonlinear Science and Numerical Simulation. 71: 50-72. DOI: 10.1016/J.Cnsns.2018.11.010 |
0.385 |
|
2019 |
Zhou T, Dowell E, Feng S. Computational investigation of wind tunnel wall effects on buffeting flow and lock-in for an airfoil at high angle of attack Aerospace Science and Technology. 95: 105492. DOI: 10.1016/J.Ast.2019.105492 |
0.407 |
|
2019 |
Ding H, Huang L, Dowell E, Chen L. Stress distribution and fatigue life of nonlinear vibration of an axially moving beam Science China Technological Sciences. 62: 1123-1133. DOI: 10.1007/S11431-017-9283-4 |
0.36 |
|
2018 |
Wang ZH, Belyaev IV, Zhang XZ, Bi CX, Faranosov GA, Dowell EH. The sound field of a rotating dipole in a plug flow. The Journal of the Acoustical Society of America. 143: 2099. PMID 29716306 DOI: 10.1121/1.5030926 |
0.374 |
|
2018 |
Dowell E. Modal damping in a finite element model (L). The Journal of the Acoustical Society of America. 140: 2288. PMID 27794287 DOI: 10.1121/1.4964341 |
0.349 |
|
2018 |
Li Z, Zhang P, Pan T, Li Q, Zhang J, Dowell EH. Catastrophe-Theory-Based Modeling of Airfoil-Stall Boundary at Low Reynolds Numbers Aiaa Journal. 56: 36-45. DOI: 10.2514/1.J056048 |
0.384 |
|
2018 |
Padmanabhan MA, Dowell EH, Pasiliao CL. Computational Study of Aeroelastic Limit Cycles due to Localized Structural Nonlinearities Journal of Aircraft. 55: 1531-1541. DOI: 10.2514/1.C034645 |
0.353 |
|
2018 |
Zhou T, Feng S, Dowell EH. Buffeting and Lock in of an Airfoil at High Angle of Attack Journal of Aircraft. 55: 771-780. DOI: 10.2514/1.C034432 |
0.348 |
|
2018 |
Moradi M, Sadeghi MH, Dowell EH. Experimental and Theoretical Flutter Investigation for a Range of Wing Wind-Tunnel Models Journal of Aircraft. 55: 891-897. DOI: 10.2514/1.C034311 |
0.308 |
|
2018 |
Abad MJS, Mahmoudi M, Dowell E. Novel Technique for Dynamic Analysis of Shear-Frames Based on Energy Balance Equations Scientia Iranica. 0-0. DOI: 10.24200/Sci.2018.20790 |
0.385 |
|
2018 |
McHugh K, Dowell E. Nonlinear Responses of Inextensible Cantilever and Free–Free Beams Undergoing Large Deflections Journal of Applied Mechanics. 85. DOI: 10.1115/1.4039478 |
0.418 |
|
2018 |
Ding H, Dowell EH, Chen L. Transmissibility of Bending Vibration of an Elastic Beam Journal of Vibration and Acoustics. 140. DOI: 10.1115/1.4038733 |
0.371 |
|
2018 |
Kasem MM, Dowell EH. A study of the natural modes of vibration and aeroelastic stability of a plate with a piezoelectric material Smart Materials and Structures. 27: 075043. DOI: 10.1088/1361-665X/Aac8A7 |
0.347 |
|
2018 |
Culver D, Dowell E. On modal cross-coupling in the asymptotic modal limit Journal of Sound and Vibration. 416: 172-191. DOI: 10.1016/J.Jsv.2017.11.039 |
0.333 |
|
2018 |
Tang D, Dowell E. Aeroelastic response and energy harvesting from a cantilevered piezoelectric laminated plate Journal of Fluids and Structures. 76: 14-36. DOI: 10.1016/J.Jfluidstructs.2017.09.007 |
0.368 |
|
2018 |
Wu Q, Zhang W, Dowell E. Detecting multi-pulse chaotic dynamics of high-dimensional non-autonomous nonlinear system for circular mesh antenna International Journal of Non-Linear Mechanics. 102: 25-40. DOI: 10.1016/J.Ijnonlinmec.2018.03.006 |
0.38 |
|
2018 |
Askarian AR, Abtahi H, Firouz-Abadi RD, Haddadpour H, Dowell EH. Bending-torsional instability of a viscoelastic cantilevered pipe conveying pulsating fluid with an inclined terminal nozzle Journal of Mechanical Science and Technology. 32: 2999-3008. DOI: 10.1007/S12206-018-0603-0 |
0.311 |
|
2018 |
Zhang W, Wu QL, Yao MH, Dowell EH. Analysis on global and chaotic dynamics of nonlinear wave equations for truss core sandwich plate Nonlinear Dynamics. 94: 21-37. DOI: 10.1007/S11071-018-4343-6 |
0.37 |
|
2017 |
Padmanabhan MA, Dowell EH. Calculation of Aeroelastic Limit Cycles due to Localized Nonlinearity and Static Preload Aiaa Journal. 55: 2762-2772. DOI: 10.2514/1.J055505 |
0.368 |
|
2017 |
Wei Y, Dowell EH, Chen Z, Jiao Y, Zhang Z. Influence of Geometry on Rotordynamic Coefficients of Brush Seal International Journal of Turbo & Jet-Engines. 34. DOI: 10.1515/Tjj-2015-0063 |
0.346 |
|
2017 |
Wei Y, Chen Z, Dowell EH. Nonlinear Characteristics Analysis of a Rotor-Bearing-Brush Seal System International Journal of Structural Stability and Dynamics. 18: 1850063. DOI: 10.1142/S0219455418500633 |
0.405 |
|
2017 |
Culver DR, Dowell EH. High Frequency Analysis of a Point-Coupled Parallel Plate System Journal of Vibration and Acoustics. 139. DOI: 10.1115/1.4036212 |
0.343 |
|
2017 |
Eugeni M, Mastroddi F, Dowell EH. Normal form analysis of a forced aeroelastic plate Journal of Sound and Vibration. 390: 141-163. DOI: 10.1016/J.Jsv.2016.12.001 |
0.448 |
|
2017 |
Verstraelen E, Dimitriadis G, Rossetto GDB, Dowell EH. Two-domain and three-domain limit cycles in a typical aeroelastic system with freeplay in pitch Journal of Fluids and Structures. 69: 89-107. DOI: 10.1016/J.Jfluidstructs.2016.11.019 |
0.355 |
|
2017 |
Al-Mashhadani WJ, Dowell EH, Wasmi HR, Al-Asadi AA. Aeroelastic response and limit cycle oscillations for wing-flap-tab section with freeplay in tab Journal of Fluids and Structures. 68: 403-422. DOI: 10.1016/J.Jfluidstructs.2016.11.017 |
0.487 |
|
2017 |
Ding H, Tan X, Dowell EH. Natural frequencies of a super-critical transporting Timoshenko beam European Journal of Mechanics - a/Solids. 66: 79-93. DOI: 10.1016/J.Euromechsol.2017.06.007 |
0.385 |
|
2017 |
Culver D, Dowell E. Iterative techniques for analyzing nonlinear vibrating dynamical systems in the frequency domain Nonlinear Dynamics. 91: 2113-2140. DOI: 10.1007/S11071-017-4005-0 |
0.432 |
|
2016 |
Padmanabhan MA, Dowell EH, Thomas JP, Pasiliao CL. Store-Induced Limit-Cycle Oscillations Due to Nonlinear Wing-Store Attachment Journal of Aircraft. 53: 778-789. DOI: 10.2514/1.C033577 |
0.421 |
|
2016 |
Lin H, Wang S, Dowell EH, Dong J. Bifurcation Observation of Combining Spiral Gear Transmission Based on Parameter Domain Structure Analysis Mathematical Problems in Engineering. 2016: 1-13. DOI: 10.1155/2016/3738508 |
0.364 |
|
2016 |
Sayag MR, Dowell EH. Linear Versus Nonlinear Response of a Cantilevered Beam Under Harmonic Base Excitation: Theory and Experiment Journal of Applied Mechanics. 83. DOI: 10.1115/1.4034117 |
0.417 |
|
2016 |
Dowell E, McHugh K. Equations of Motion for an Inextensible Beam Undergoing Large Deflections Journal of Applied Mechanics, Transactions Asme. 83. DOI: 10.1115/1.4032795 |
0.332 |
|
2016 |
Culver D, Dowell E. High frequency analysis of a plate carrying a concentrated nonlinear spring–mass system Journal of Sound and Vibration. 379: 84-105. DOI: 10.1016/J.Jsv.2016.05.048 |
0.399 |
|
2016 |
Ganji HF, Dowell EH. Panel flutter prediction in two dimensional flow with enhanced piston theory Journal of Fluids and Structures. 63: 97-102. DOI: 10.1016/J.Jfluidstructs.2016.03.003 |
0.401 |
|
2016 |
Besem FM, Thomas JP, Kielb RE, Dowell EH. An aeroelastic model for vortex-induced vibrating cylinders subject to frequency lock-in Journal of Fluids and Structures. 61: 42-59. DOI: 10.1016/J.Jfluidstructs.2015.10.009 |
0.445 |
|
2016 |
Balajewicz M, Tezaur I, Dowell E. Minimal subspace rotation on the Stiefel manifold for stabilization and enhancement of projection-based reduced order models for the compressible Navier–Stokes equations Journal of Computational Physics. 321: 224-241. DOI: 10.1016/J.Jcp.2016.05.037 |
0.808 |
|
2016 |
Dowell E. Hamilton’s principle and Hamilton’s equations with holonomic and non-holonomic constraints Nonlinear Dynamics. 88: 1093-1097. DOI: 10.1007/S11071-016-3297-9 |
0.326 |
|
2016 |
Chueshov I, Dowell EH, Lasiecka I, Webster JT. Nonlinear Elastic Plate in a Flow of Gas: Recent Results and Conjectures Applied Mathematics and Optimization. 1-26. DOI: 10.1007/S00245-016-9349-1 |
0.419 |
|
2015 |
Mannarino A, Dowell EH. Reduced-Order Models for Computational-Fluid-Dynamics-Based Nonlinear Aeroelastic Problems Aiaa Journal. 53: 2671-2685. DOI: 10.2514/1.J053775 |
0.424 |
|
2015 |
Tang D, Gibbs SC, Dowell EH. Nonlinear Aeroelastic Analysis with Inextensible Plate Theory Including Correlation with Experiment Aiaa Journal. 53: 1299-1308. DOI: 10.2514/1.J053385 |
0.432 |
|
2015 |
Padmanabhan MA, Dowell EH. Landing gear design/maintenance analysis for nonlinear shimmy Journal of Aircraft. 52: 1707-1710. DOI: 10.2514/1.C033027 |
0.419 |
|
2015 |
Gibbs SC, Wang I, Dowell EH. Stability of rectangular plates in subsonic flow with various boundary conditions Journal of Aircraft. 52: 439-451. DOI: 10.2514/1.C032738 |
0.804 |
|
2015 |
Goldman BD, Dowell EH, Scott RC. Aeroelastic stability of thermal protection system for inflatable aerodynamic decelerator Journal of Spacecraft and Rockets. 52: 144-156. DOI: 10.2514/1.A33001 |
0.655 |
|
2015 |
Mannarino A, Dowell EH, Mantegazza P. An adaptive controller for nonlinear flutter suppression and free-play compensation Journal of Vibration and Control. 23: 2269-2290. DOI: 10.1177/1077546315613935 |
0.379 |
|
2015 |
Xie D, Xu M, Dai H, Dowell EH. Proper orthogonal decomposition method for analysis of nonlinear panel flutter with thermal effects in supersonic flow Journal of Sound and Vibration. 337: 263-283. DOI: 10.1016/J.Jsv.2014.10.038 |
0.416 |
|
2014 |
Goldman BD, Dowell EH. Nonlinear oscillations of a fluttering plate resting on a unidirectional elastic foundation Aiaa Journal. 52: 2364-2368. DOI: 10.2514/1.J053290 |
0.642 |
|
2014 |
Padmanabhan MA, Pasiliao CL, Dowell EH. Simulation of aeroelastic limit-cycle oscillations of aircraft wings with stores Aiaa Journal. 52: 2291-2299. DOI: 10.2514/1.J052843 |
0.429 |
|
2014 |
Tang D, Dowell EH. Effects of a Free-to-Roll Fuselage on Wing Flutter: Theory and Experiment Aiaa Journal. 52: 2625-2632. DOI: 10.2514/1.J052562 |
0.422 |
|
2014 |
Raveh DE, Dowell EH. Aeroelastic Responses of Elastically Suspended Airfoil Systems in Transonic Buffeting Flows Aiaa Journal. 52: 926-934. DOI: 10.2514/1.J052185 |
0.388 |
|
2014 |
Tang D, Dowell EH. Experimental Aerodynamic Response for an Oscillating Airfoil in Buffeting Flow Aiaa Journal. 52: 1170-1179. DOI: 10.2514/1.J052077 |
0.393 |
|
2014 |
Xie D, Xu M, Dowell EH. Proper Orthogonal Decomposition Reduced-Order Model for Nonlinear Aeroelastic Oscillations Aiaa Journal. 52: 229-241. DOI: 10.2514/1.J051989 |
0.465 |
|
2014 |
Tang D, Zhao M, Dowell EH. Inextensible Beam and Plate Theory: Computational Analysis and Comparison With Experiment Journal of Applied Mechanics. 81. DOI: 10.1115/1.4026800 |
0.392 |
|
2014 |
Wu ZY, Dowell EH, Tang DM. Damping Analysis In Beams Subject To Presliding Friction Mechanics Based Design of Structures and Machines. 42: 229-243. DOI: 10.1080/15397734.2013.875858 |
0.398 |
|
2014 |
Xie D, Xu M, Dowell EH. Projection-free proper orthogonal decomposition method for a cantilever plate in supersonic flow Journal of Sound and Vibration. 333: 6190-6208. DOI: 10.1016/J.Jsv.2014.06.039 |
0.421 |
|
2014 |
Eugeni M, Dowell EH, Mastroddi F. Post-buckling longterm dynamics of a forced nonlinear beam: A perturbation approach Journal of Sound and Vibration. 333: 2617-2631. DOI: 10.1016/J.Jsv.2013.12.026 |
0.438 |
|
2014 |
Xie D, Xu M, Dai H, Dowell EH. Observation and evolution of chaos for a cantilever plate in supersonic flow Journal of Fluids and Structures. 50: 271-291. DOI: 10.1016/J.Jfluidstructs.2014.05.015 |
0.398 |
|
2014 |
Gibbs SC, Sethna A, Wang I, Tang D, Dowell E. Aeroelastic stability of a cantilevered plate in yawed subsonic flow Journal of Fluids and Structures. 49: 450-462. DOI: 10.1016/J.Jfluidstructs.2014.05.006 |
0.822 |
|
2014 |
Gibbs S, Fichera S, Zanotti A, Ricci S, Dowell EH. Flow field around the flapping flag Journal of Fluids and Structures. 48: 507-513. DOI: 10.1016/J.Jfluidstructs.2014.02.011 |
0.785 |
|
2014 |
Eftekhari S, Bakhtiari-Nejad F, Dowell E. Damage detection of an aeroelastic panel using limit cycle oscillation analysis International Journal of Non-Linear Mechanics. 58: 99-110. DOI: 10.1016/J.Ijnonlinmec.2013.09.008 |
0.323 |
|
2014 |
Yan S, Dowell EH, Lin B. Effects of nonlinear damping suspension on nonperiodic motions of a flexible rotor in journal bearings Nonlinear Dynamics. 78: 1435-1450. DOI: 10.1007/S11071-014-1526-7 |
0.398 |
|
2013 |
Nefske DJ, Sung SH, Dowell EH. Comment on "On Dowell's simplification for acoustic cavity-structure interaction and consistent alternatives [J. Acoust. Soc. Am. 127, 22-32 (2010)]". The Journal of the Acoustical Society of America. 133: 1222-4. PMID 23463994 DOI: 10.1121/1.3436549 |
0.311 |
|
2013 |
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. DOI: 10.2514/6.2013-1837 |
0.324 |
|
2013 |
Tang D, Dowell EH. Experimental Aeroelastic Response for a Freeplay Control Surface in Buffeting Flow Aiaa Journal. 51: 2852-2861. DOI: 10.2514/1.J052495 |
0.39 |
|
2013 |
Dowell EH, Bliss DB. New look at unsteady supersonic potential flow aerodynamics and piston theory Aiaa Journal. 51: 2278-2281. DOI: 10.2514/1.J052088 |
0.31 |
|
2013 |
Thomas JP, Custer CH, Dowell EH, Hall KC, Corre C. Compact implementation strategy for a harmonic balance method within implicit flow solvers Aiaa Journal. 51: 1374-1381. DOI: 10.2514/1.J051823 |
0.772 |
|
2013 |
Tang D, Dowell EH. Computational/Experimental Aeroelastic Study for a Horizontal-Tail Model with Free Play Aiaa Journal. 51: 341-352. DOI: 10.2514/1.J051781 |
0.429 |
|
2013 |
Grasch AD, Jaworski JW, Tang D, Dowell EH. Resonant frequency determination of a multistore high-altitude/long- endurance wing Aiaa Journal. 51: 1277-1283. DOI: 10.2514/1.J051499 |
0.734 |
|
2013 |
Hall KC, Ekici K, Thomas JP, Dowell EH. Harmonic balance methods applied to computational fluid dynamics problems International Journal of Computational Fluid Dynamics. 27: 52-67. DOI: 10.1080/10618562.2012.742512 |
0.445 |
|
2013 |
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. 729: 285-308. DOI: 10.1017/Jfm.2013.278 |
0.399 |
|
2012 |
Jaworski JW, Dowell EH. Scaling analysis for aeroelastic phenomena using the navier-stokes fluid model Aiaa Journal. 50: 2622-2626. DOI: 10.2514/1.J051727 |
0.714 |
|
2012 |
Balajewicz M, Dowell E. Reduced-Order Modeling of Flutter and Limit-Cycle Oscillations Using the Sparse Volterra Series Journal of Aircraft. 49: 1803-1812. DOI: 10.2514/1.C031637 |
0.801 |
|
2012 |
Wang I, Gibbs SC, Dowell EH. Aeroelastic Model of Multisegmented Folding Wings: Theory and Experiment Journal of Aircraft. 49: 911-921. DOI: 10.2514/1.C031589 |
0.805 |
|
2012 |
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. 23: 183-199. DOI: 10.1177/1045389X11432656 |
0.41 |
|
2012 |
Chad Gibbs S, Wang I, Dowell E. Theory and experiment for flutter of a rectangular plate with a fixed leading edge in three-dimensional axial flow Journal of Fluids and Structures. 34: 68-83. DOI: 10.1016/J.Jfluidstructs.2012.06.009 |
0.816 |
|
2012 |
Balajewicz M, Dowell EH. Stabilization of projection-based reduced order models of the Navier–Stokes Nonlinear Dynamics. 70: 1619-1632. DOI: 10.1007/S11071-012-0561-5 |
0.801 |
|
2011 |
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. 4424-4432. DOI: 10.4028/Www.Scientific.Net/Amm.110-116.4424 |
0.328 |
|
2011 |
Tang D, Dowell EH. Aeroelastic Response Induced by Free Play, Part 2: Theoretical/Experimental Correlation Analysis Aiaa Journal. 49: 2543-2554. DOI: 10.2514/1.J051056 |
0.385 |
|
2011 |
Tang D, Dowell EH. Aeroelastic Response Induced by Free Play, Part 1: Theory Aiaa Journal. 49: 2532-2542. DOI: 10.2514/1.J051055 |
0.401 |
|
2011 |
Wang I, Dowell EH. Structural Dynamics model of multisegmented folding wings: Theory and experiment Journal of Aircraft. 48: 2149-2160. DOI: 10.2514/1.C031509 |
0.808 |
|
2011 |
Tang D, Dowell EH. Aeroelastic Analysis and Experiment for Wing/Store Model with Stiction Nonlinearity Journal of Aircraft. 48: 1512-1530. DOI: 10.2514/1.C031151 |
0.49 |
|
2011 |
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. 4: 1181-1190. DOI: 10.1115/DETC2011-47002 |
0.317 |
|
2011 |
Dunnmon JA, Stanton SC, Mann BP, Dowell EH. Power extraction from aeroelastic limit cycle oscillations Journal of Fluids and Structures. 27: 1182-1198. DOI: 10.1016/J.Jfluidstructs.2011.02.003 |
0.431 |
|
2011 |
Eftekhari S, Bakhtiari-Nejad F, Dowell E. Bifurcation boundary analysis as a nonlinear damage detection feature: does it work? Journal of Fluids and Structures. 27: 297-310. DOI: 10.1016/J.Jfluidstructs.2010.11.006 |
0.345 |
|
2011 |
Raveh D, Dowell E. Frequency lock-in phenomenon for oscillating airfoils in buffeting flows Journal of Fluids and Structures. 27: 89-104. DOI: 10.1016/J.Jfluidstructs.2010.10.001 |
0.388 |
|
2010 |
Tang D, Grasch A, Dowell EH. Gust Response for Flexibly Suspended High-Aspect Ratio Wings Aiaa Journal. 48: 2430-2444. DOI: 10.2514/1.J050309 |
0.471 |
|
2010 |
Attar PJ, Tang D, Dowell EH. Nonlinear Aeroelastic Study for Folding Wing Structures Aiaa Journal. 48: 2187-2195. DOI: 10.2514/1.44868 |
0.766 |
|
2010 |
Tang D, Dowell EH. Aeroelastic Airfoil with Free Play at Angle of Attack with Gust Excitation Aiaa Journal. 48: 427-442. DOI: 10.2514/1.44538 |
0.453 |
|
2010 |
Dowell EH. Transonic Unsteady Potential Flow: Scaling Analysis of Linear and Nonlinear Dynamics Aiaa Journal. 48: 1017-1020. DOI: 10.2514/1.40426 |
0.388 |
|
2010 |
Thomas JP, Dowell EH, Hall KC. Using automatic differentiation to create a nonlinear reduced-order-model aerodynamic solver Aiaa Journal. 48: 19-24. DOI: 10.2514/1.36414 |
0.42 |
|
2009 |
Dowell EH, Thomas JP, Hall KC, Denegri CM. Theoretical predictions of F-16 fighter limit cycle oscillations for flight flutter testing Journal of Aircraft. 46: 1667-1672. DOI: 10.2514/1.42352 |
0.364 |
|
2009 |
Liska S, Dowell EH. Continuum Aeroelastic Model for a Folding-Wing Configuration Aiaa Journal. 47: 2350-2358. DOI: 10.2514/1.40475 |
0.375 |
|
2009 |
Jaworski JW, Dowell EH. Comparison of Theoretical Structural Models with Experiment for a High-Aspect-Ratio Aeroelastic Wing Journal of Aircraft. 46: 708-713. DOI: 10.2514/1.39244 |
0.751 |
|
2009 |
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. 46: 2069-2076. DOI: 10.2514/1.30703 |
0.386 |
|
2009 |
Tang D, Dowell EH. Flutter/LCO suppression for high-aspect ratio wings The Aeronautical Journal. 113: 409-416. DOI: 10.1017/S0001924000003079 |
0.466 |
|
2008 |
Tang D, Dowell EH. Theoretical and Experimental Aeroelastic Study for Folding Wing Structures Journal of Aircraft. 45: 1136-1147. DOI: 10.2514/1.32754 |
0.411 |
|
2008 |
Attar PJ, Dowell EH, Tang D. Delta Wing with Store Limit-Cycle-Oscillation Modeling Using a High-Fidelity Structural Model Journal of Aircraft. 45: 1054-1061. DOI: 10.2514/1.32217 |
0.741 |
|
2008 |
Jaworski J, Dowell E. Free vibration of a cantilevered beam with multiple steps: Comparison of several theoretical methods with experiment Journal of Sound and Vibration. 312: 713-725. DOI: 10.1016/J.Jsv.2007.11.010 |
0.731 |
|
2008 |
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. DOI: 10.1016/J.Jcp.2008.02.028 |
0.427 |
|
2007 |
Jaworski JW, Dowell EH. Supersonic Indicial Lift Functions from Transform Methods Aiaa Journal. 45: 2106-2111. DOI: 10.2514/1.28144 |
0.684 |
|
2007 |
Tang D, Dowell EH. Aerodynamic Loading for an Airfoil with an Oscillating Gurney Flap Journal of Aircraft. 44: 1245-1257. DOI: 10.2514/1.26440 |
0.414 |
|
2007 |
Liu L, Dowell E, Thomas J. A high dimensional harmonic balance approach for an aeroelastic airfoil with cubic restoring forces Journal of Fluids and Structures. 23: 351-363. DOI: 10.1016/J.Jfluidstructs.2006.09.005 |
0.412 |
|
2007 |
Liu L, Dowell EH, Hall KC. A novel harmonic balance analysis for the Van Der Pol oscillator International Journal of Non-Linear Mechanics. 42: 2-12. DOI: 10.1016/J.Ijnonlinmec.2006.09.004 |
0.375 |
|
2006 |
Tang D, Dowell EH. Aerodyamic Flow Control of an Airfoil with Small Trailing-Edge Strips Journal of Aircraft. 43: 1854-1866. DOI: 10.2514/1.18969 |
0.394 |
|
2006 |
Attar PJ, Dowell EH. Stochastic Analysis of a Nonlinear Aeroelastic Model Using the Response Surface Method Journal of Aircraft. 43: 1044-1052. DOI: 10.2514/1.17525 |
0.715 |
|
2006 |
Attar PJ, Dowell EH, White JR, Thomas JP. Reduced Order Nonlinear System Identification Methodology Aiaa Journal. 44: 1895-1904. DOI: 10.2514/1.16221 |
0.74 |
|
2006 |
Tang D, Dowell EH. Flutter and Limit-Cycle Oscillations for a Wing-Store Model with Freeplay Journal of Aircraft. 43: 487-503. DOI: 10.2514/1.12650 |
0.486 |
|
2006 |
Tang D, Attar P, Dowell EH. Flutter/Limit Cycle Oscillation Analysis and Experiment for Wing-Store Model Aiaa Journal. 44: 1662-1675. DOI: 10.2514/1.12634 |
0.759 |
|
2006 |
Thomas JP, Dowell EH, Hall KC. Static/dynamic correction approach for reduced-order modeling of unsteady aerodynamics Journal of Aircraft. 43: 865-878. DOI: 10.2514/1.12349 |
0.42 |
|
2006 |
Tang D, Dowell EH. Experimental and theoretical study of gust response for a wing–store model with freeplay Journal of Sound and Vibration. 295: 659-684. DOI: 10.1016/J.Jsv.2006.01.024 |
0.457 |
|
2006 |
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. 215: 298-320. DOI: 10.1016/J.Jcp.2005.10.026 |
0.712 |
|
2006 |
Li A, Dowell EH. Modal reduction of mathematical models of biological molecules Journal of Computational Physics. 211: 262-288. DOI: 10.1016/J.Jcp.2005.05.021 |
0.686 |
|
2006 |
Tang D, Attar P, Li A, Dowell EH. Complex Dynamics of a Pyranose Ring Structure Molecule Attached to an Atomic Force Microscope Nonlinear Dynamics. 45: 283-303. DOI: 10.1007/S11071-006-0508-9 |
0.787 |
|
2005 |
Thomas JP, Hall KC, Dowell EH. Discrete Adjoint Approach for Modeling Unsteady Aerodynamic Design Sensitivities Aiaa Journal. 43: 1931-1936. DOI: 10.2514/1.731 |
0.426 |
|
2005 |
Attar PJ, Dowell EH, White JR. Modeling Delta Wing Limit-Cycle Oscillations Using a High-Fidelity Structural Model Journal of Aircraft. 42: 1209-1217. DOI: 10.2514/1.11325 |
0.744 |
|
2005 |
Liu L, Dowell EH. Harmonic Balance Approach for an Airfoil with a Freeplay Control Surface Aiaa Journal. 43: 802-815. DOI: 10.2514/1.10973 |
0.412 |
|
2005 |
Attar PJ, Dowell EH. A reduced order system ID approach to the modelling of nonlinear structural behavior in aeroelasticity Journal of Fluids and Structures. 21: 531-542. DOI: 10.1016/J.Jfluidstructs.2005.08.012 |
0.731 |
|
2005 |
Xie J, Ding W, Dowell EH, Virgin LN. Hopf-flip bifurcation of high dimensional maps and application to vibro-impact systems Acta Mechanica Sinica/Lixue Xuebao. 21: 402-410. DOI: 10.1007/S10409-005-0045-7 |
0.31 |
|
2004 |
Thomas JP, Dowell EH, Hall KC. Modeling Viscous Transonic Limit Cycle Oscillation Behavior Using a Harmonic Balance Approach Journal of Aircraft. 41: 1266-1274. DOI: 10.2514/1.9839 |
0.41 |
|
2004 |
Kholodar DB, Dowell EH, Thomas JP, Hall KC. Limit Cycle Oscillation of a Typical Airfoil in Transonic Flow Journal of Aircraft. 41: 1067-1072. DOI: 10.2514/1.618 |
0.809 |
|
2004 |
Kholodar DB, Dowell EH, Thomas JP, Hall KC. Improved Understanding of Transonic Flutter: A Three-Parameter Flutter Surface Journal of Aircraft. 41: 911-917. DOI: 10.2514/1.467 |
0.79 |
|
2004 |
Tang D, Dowell EH. Dynamic Analysis of a Protein-Ligand Molecular Chain Attached to an Atomic Force Microscope Journal of Vibration and Acoustics. 126: 496-513. DOI: 10.1115/1.1804999 |
0.415 |
|
2004 |
Tang D, Dowell EH. Reduced Order Model Analysis for Two-Dimensional Molecular Dynamic Chain Structure Attached to an Atomic Force Microscope Journal of Dynamic Systems, Measurement, and Control. 126: 531-546. DOI: 10.1115/1.1789969 |
0.43 |
|
2004 |
Liu L, Dowell EH. The Secondary Bifurcation of an Aeroelastic Airfoil Motion: Effect of High Harmonics Nonlinear Dynamics. 37: 31-49. DOI: 10.1023/B:Nody.0000040033.85421.4D |
0.404 |
|
2004 |
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. 269: 853-874. DOI: 10.1016/S0022-460X(03)00180-9 |
0.36 |
|
2004 |
Li A, Dowell E. Asymptotic modal analysis of dynamical systems: the effect of modal cross-correlation Journal of Sound and Vibration. 276: 65-80. DOI: 10.1016/J.Jsv.2003.07.031 |
0.308 |
|
2004 |
Tang D, Li A, Dowell E. Transient response study on rolling effectiveness of multiple control surfaces Journal of Fluids and Structures. 19: 621-634. DOI: 10.1016/J.Jfluidstructs.2004.01.006 |
0.7 |
|
2004 |
Tang D, Dowell E. Effects of geometric structural nonlinearity on flutter and limit cycle oscillations of high-aspect-ratio wings Journal of Fluids and Structures. 19: 291-306. DOI: 10.1016/J.Jfluidstructs.2003.10.007 |
0.457 |
|
2004 |
Dowell E, Thomas J, Hall K. Transonic limit cycle oscillation analysis using reduced order aerodynamic models Journal of Fluids and Structures. 19: 17-27. DOI: 10.1016/J.Jfluidstructs.2003.07.018 |
0.445 |
|
2004 |
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. 201: 723-752. DOI: 10.1016/J.Jcp.2004.06.016 |
0.801 |
|
2003 |
Epureanu BI, Dowell EH. Compact Methodology for Computing Limit-Cycle Oscillations in Aeroelasticity Journal of Aircraft. 40: 955-963. DOI: 10.2514/2.6880 |
0.41 |
|
2003 |
Thomas JP, Dowell EH, Hall KC. Three-Dimensional Transonic Aeroelasticity Using Proper Orthogonal Decomposition-Based Reduced-Order Models Journal of Aircraft. 40: 544-551. DOI: 10.2514/2.3128 |
0.446 |
|
2003 |
Kholodar DB, Thomas JP, Dowell EH, Hall KC. Parametric Study of Flutter for an Airfoil in Inviscid Transonic Flow Journal of Aircraft. 40: 303-313. DOI: 10.2514/2.3094 |
0.813 |
|
2003 |
Tang D, Li A, Dowell EH. Experimental and Theoretical Study on Rolling Effectiveness of Multiple Control Surfaces Aiaa Journal. 41: 160-167. DOI: 10.2514/2.1944 |
0.656 |
|
2003 |
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. 70: 328-338. DOI: 10.1115/1.1558079 |
0.403 |
|
2003 |
Epureanu BI, Dowell EH. Localized basis function method for computing limit cycle oscillations Nonlinear Dynamics. 31: 151-166. DOI: 10.1023/A:1022081101766 |
0.352 |
|
2003 |
Attar P, Dowell E, Tang D. 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. 17: 243-259. DOI: 10.1016/S0889-9746(02)00123-8 |
0.743 |
|
2002 |
Tang D, Dowell EH. Limit-Cycle Hysteresis Response for a High-Aspect-Ratio Wing Model Journal of Aircraft. 39: 885-888. DOI: 10.2514/2.3009 |
0.435 |
|
2002 |
Dowell EH, Tang D. Nonlinear Aeroelasticity and Unsteady Aerodynamics Aiaa Journal. 40: 1697-1707. DOI: 10.2514/2.1853 |
0.432 |
|
2002 |
Juang J, Kholodar D, Dowell EH. System Identification of a Vortex Lattice Aerodynamic Model Aiaa Journal. 40: 1187-1196. DOI: 10.2514/2.1770 |
0.796 |
|
2002 |
Thomas JP, Dowell EH, Hall KC. Nonlinear Inviscid Aerodynamic Effects on Transonic Divergence, Flutter, and Limit-Cycle Oscillations Aiaa Journal. 40: 638-646. DOI: 10.2514/2.1720 |
0.411 |
|
2002 |
Tang D, Dowell EH. Experimental and Theoretical Study of Gust Response for High-Aspect-Ratio Wing Aiaa Journal. 40: 419-429. DOI: 10.2514/2.1691 |
0.463 |
|
2002 |
Epureanu BI, Dowell EH, Hall KC. Mach number influence on reduced-order models of inviscid potential flows in turbomachinery Journal of Fluids Engineering, Transactions of the Asme. 124: 977-987. DOI: 10.1115/1.1511165 |
0.454 |
|
2002 |
Trickley ST, Virgin LN, Dowell EH. The stability of limit-cycle oscillations in a nonlinear aeroelastic system Proceedings of the Royal Society a: Mathematical, Physical and Engineering Sciences. 458: 2203-2226. DOI: 10.1098/Rspa.2002.0965 |
0.412 |
|
2002 |
Tang D, Dowell EH. Limit cycle oscillations of two-dimensional panels in low subsonic flow International Journal of Non-Linear Mechanics. 37: 1199-1209. DOI: 10.1016/S0020-7462(01)00140-8 |
0.445 |
|
2002 |
TANG D, HENRY J, DOWELL E. EFFECTS OF STEADY ANGLE OF ATTACK ON NONLINEAR GUST RESPONSE OF A DELTA WING MODEL Journal of Fluids and Structures. 16: 1093-1110. DOI: 10.1006/Jfls.2002.0465 |
0.461 |
|
2001 |
Tang D, Dowell EH. Experimental and Theoretical Study on Aeroelastic Response of High-Aspect-Ratio Wings Aiaa Journal. 39: 1430-1441. DOI: 10.2514/2.1484 |
0.47 |
|
2001 |
Tang D, Kholodar D, Juang J, Dowell EH. System Identification and Proper Orthogonal Decomposition Method Applied to Unsteady Aerodynamics Aiaa Journal. 39: 1569-1576. DOI: 10.2514/2.1482 |
0.799 |
|
2001 |
Tang D, Dowell EH. Effects of Angle of Attack on Nonlinear Flutter of a Delta Wing Aiaa Journal. 39: 15-21. DOI: 10.2514/2.1296 |
0.431 |
|
2001 |
Dowell EH, Hall KC. MODELING OFFLUID-STRUCTUREINTERACTION Annual Review of Fluid Mechanics. 33: 445-490. DOI: 10.1146/Annurev.Fluid.33.1.445 |
0.379 |
|
2001 |
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. 1. DOI: 10.1115/2001-GT-0434 |
0.351 |
|
2001 |
Dowell EH, Tang D. Mathematical model of a nanopaddle oscillator Journal of Applied Physics. 90: 5606-5611. DOI: 10.1063/1.1415535 |
0.391 |
|
2001 |
Epureanu BI, Hall KC, Dowell EH. Reduced-order models of unsteady viscous flows in turbomachinery using viscous-inviscid coupling Journal of Fluids and Structures. 15: 255-273. DOI: 10.1006/Jfls.2000.0334 |
0.455 |
|
2000 |
Hall KC, Thomas JP, Dowell EH. Proper Orthogonal Decomposition Technique for Transonic Unsteady Aerodynamic Flows Aiaa Journal. 38: 1853-1862. DOI: 10.2514/2.867 |
0.426 |
|
2000 |
Florea R, Hall KC, Dowell EH. Eigenmode Analysis and Reduced-Order Modeling of Unsteady Transonic Potential Flow Around Airfoils Journal of Aircraft. 37: 454-462. DOI: 10.2514/2.2619 |
0.409 |
|
2000 |
Tang D, Henry JK, Dowell EH. Nonlinear Aeroelastic Response of Delta Wing to Periodic Gust Journal of Aircraft. 37: 155-164. DOI: 10.2514/2.2575 |
0.478 |
|
2000 |
Tang D, Kholodar D, Dowell EH. Nonlinear Response of Airfoil Section with Control Surface Freeplay to Gust Loads Aiaa Journal. 38: 1543-1557. DOI: 10.2514/2.1176 |
0.83 |
|
2000 |
Kholodar D, Dowell E. 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. 1. DOI: 10.1515/Ijnsns.2000.1.3.153 |
0.783 |
|
2000 |
Dowell EH. Nonlinear dynamics of aeroelastic systems The Journal of the Acoustical Society of America. 107: 2823-2823. DOI: 10.1121/1.429108 |
0.459 |
|
2000 |
Epureanu BI, Dowell EH. Optimal multi-dimensional OGY controller Physica D: Nonlinear Phenomena. 139: 87-96. DOI: 10.1016/S0167-2789(99)00201-8 |
0.329 |
|
2000 |
Epureanu BI, Dowell EH, Hall KC. Reduced-order models of unsteady transonic viscous flows in turbomachinery Journal of Fluids and Structures. 14: 1215-1234. DOI: 10.1006/Jfls.2000.0320 |
0.465 |
|
1999 |
Kholodar DB, Dowell EH. Behavior of Airfoil with Control Surface Freeplay for Nonzero Angles of Attack Aiaa Journal. 37: 651-653. DOI: 10.2514/2.766 |
0.762 |
|
1999 |
Tang D, Dowell EH, Hall KC. Limit Cycle Oscillations of a Cantilevered Wing in Low Subsonic Flow Aiaa Journal. 37: 364-371. DOI: 10.2514/2.717 |
0.454 |
|
1999 |
Tang D, Henry JK, Dowell EH. Limit Cycle Oscillations of Delta Wing Models in Low Subsonic Flow Aiaa Journal. 37: 1355-1362. DOI: 10.2514/2.627 |
0.485 |
|
1998 |
Tang D, Dowell EH, Peters DA. Reduced Order Aerodynamic Models Based Upon Inflow Eigenmodes Journal of the American Helicopter Society. 43: 342-351. DOI: 10.4050/Jahs.43.342 |
0.337 |
|
1998 |
Tang D, Dowell EH. Unsteady Aerodynamic Forces and Aeroelastic Response for External Store of an Aircraft Journal of Aircraft. 35: 678-687. DOI: 10.2514/2.2377 |
0.444 |
|
1998 |
Vipperman JS, Clark RL, Conner M, Dowell EH. Experimental active control of a typical section using a trailing-edge flap Journal of Aircraft. 35: 224-229. DOI: 10.2514/2.2312 |
0.315 |
|
1998 |
Tang D, Conner MD, Dowell EH. Reduced-Order Aerodynamic Model and Its Application to a Nonlinear Aeroelastic System Journal of Aircraft. 35: 332-338. DOI: 10.2514/2.2304 |
0.45 |
|
1998 |
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. 8: 521-533. DOI: 10.1142/S0218127498000334 |
0.355 |
|
1998 |
Reynolds RR, Dowell EH. The Transient Response of Structures Using Asymptotic Modal Analysis Journal of Applied Mechanics. 65: 258-265. DOI: 10.1115/1.2789034 |
0.37 |
|
1998 |
Hu H, Dowell EH, Virgin LN. Resonances of a Harmonically Forced Duffing Oscillator with Time Delay State Feedback Nonlinear Dynamics. 15: 311-327. DOI: 10.1023/A:1008278526811 |
0.351 |
|
1998 |
Virgin LN, Dowell EH, Conner MD. On the evolution of deterministic non-periodic behavior of an airfoil International Journal of Non-Linear Mechanics. 34: 499-514. DOI: 10.1016/S0020-7462(98)00038-9 |
0.367 |
|
1998 |
Hu HY, Dowell EH, Virgin LN. Stability estimation of high dimensional vibrating systems under state delay feedback control Journal of Sound and Vibration. 214: 497-511. DOI: 10.1006/Jsvi.1998.1548 |
0.334 |
|
1998 |
Dowell E, Tang D. THE HIGH-FREQUENCY RESPONSE OF A PLATE CARRYING A CONCENTRATED MASS/SPRING SYSTEM Journal of Sound and Vibration. 213: 843-863. DOI: 10.1006/Jsvi.1998.1520 |
0.328 |
|
1998 |
DOWELL E. COMMENTS ON THE NONLINEAR VIBRATIONS OF CYLINDRICAL SHELLS Journal of Fluids and Structures. 12: 1087-1089. DOI: 10.1006/Jfls.1998.0183 |
0.345 |
|
1998 |
Tang D, Dowell EH, Virgin LN. Limit cycle behavior of an airfoil with a control surface Journal of Fluids and Structures. 12: 839-858. DOI: 10.1006/Jfls.1998.0174 |
0.429 |
|
1997 |
Tang D, Dowell EH. Nonlinear Rotor Aeroelastic Analysis with Stall and Advanced Wake Dynamics Journal of Aircraft. 34: 679-687. DOI: 10.2514/2.2229 |
0.443 |
|
1997 |
Dowell EH, Hall KC, Romanowski MC. Eigenmode Analysis in Unsteady Aerodynamics: Reduced Order Models Applied Mechanics Reviews. 50: 371-386. DOI: 10.1115/1.3101718 |
0.453 |
|
1997 |
Epureanu BI, Dowell EH. System identification for the Ott-Grebogi-Yorke controller design Physical Review E. 56: 5327-5331. DOI: 10.1103/Physreve.56.5327 |
0.339 |
|
1997 |
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. 11: 89-109. DOI: 10.1006/Jfls.1996.0068 |
0.438 |
|
1997 |
Conner MD, Tang DM, Dowell EH, Virgin LN. Nonlinear aeroelasticity of an airfoil with control surface freeplay 35th Aerospace Sciences Meeting and Exhibit. |
0.328 |
|
1996 |
Tang D, Dowell EH. Damping prediction for hingeless rotor aeroelastic stability with experimental correlation Journal of Aircraft. 33: 1071-1078. DOI: 10.2514/3.47059 |
0.405 |
|
1996 |
Frampton KD, Clark RL, Dowell EH. State-space modeling for aeroelastic panels with linearized potential flow aerodynamic loading Journal of Aircraft. 33: 816-822. DOI: 10.2514/3.47019 |
0.384 |
|
1996 |
Frampton KD, Clark RL, Dowell EH. Active control of panel flutter with piezoelectric transducers Journal of Aircraft. 33: 768-774. DOI: 10.2514/3.47013 |
0.366 |
|
1996 |
Cizmas PGA, Tang D, Dowell EH. Flow about a slotted cylinder-airfoil combination in a wind tunnel Journal of Aircraft. 33: 716-721. DOI: 10.2514/3.47006 |
0.4 |
|
1996 |
Tang DM, Cizmas PGA, Dowell EH. Experiments and analysis for a gust generator in a wind tunnel Journal of Aircraft. 33: 139-148. DOI: 10.2514/3.46914 |
0.364 |
|
1996 |
Conner MD, Virgin LN, Dowell EH. Accurate numerical integration of state-space models for aeroelastic systems with free play Aiaa Journal. 34: 2202-2205. DOI: 10.2514/3.13377 |
0.324 |
|
1996 |
Dowell EH. Eigenmode analysis in unsteady aerodynamics - Reduced-order models Aiaa Journal. 34: 1578-1583. DOI: 10.2514/3.13274 |
0.425 |
|
1996 |
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. 31: 931-939. DOI: 10.1016/S0020-7462(96)00114-X |
0.338 |
|
1996 |
Dowell E. COMMENT OF ENERGY FLOW PREDICTIONS IN A STRUCTURE OF RIGIDLY JOINED BEAMS USING RECEPTANCE THEORY Journal of Sound and Vibration. 194: 445-447. DOI: 10.1006/Jsvi.1996.0368 |
0.319 |
|
1996 |
Tang D, Dowell E. NONLINEAR RESPONSE OF A NON-ROTATING ROTOR BLADE TO A PERIODIC GUST Journal of Fluids and Structures. 10: 721-742. DOI: 10.1006/Jfls.1996.0050 |
0.438 |
|
1996 |
Tang D, Dowell E. COMMENTS ON THE ONERA STALL AERODYNAMIC MODEL AND ITS IMPACT ON AEROELASTIC STABILITY Journal of Fluids and Structures. 10: 353-366. DOI: 10.1006/Jfls.1996.0023 |
0.422 |
|
1995 |
Tang DM, Dowell EH. Response of a Nonrotating Rotor Blade to Lateral Turbulence Part I: Theory Journal of Aircraft. 32: 145-153. DOI: 10.2514/3.56920 |
0.455 |
|
1995 |
Tang DM, Dowell EH. Experimental investigation of three-dimensional dynamic stall model oscillating in pitch Journal of Aircraft. 32: 1062-1071. DOI: 10.2514/3.46837 |
0.443 |
|
1995 |
Tang DM, Dowell EH. Response of a nonrotating rotor blade to lateral turbulence Part II: Experiment Journal of Aircraft. 32: 154-160. DOI: 10.2514/3.46695 |
0.382 |
|
1995 |
Epstein RJ, Srinivasan R, Dowell EH. Flutter of an infinitely long panel in a duct Aiaa Journal. 33: 109-115. DOI: 10.2514/3.12339 |
0.37 |
|
1995 |
Franzoni LP, Dowell EH. On the accuracy of modal analysis in reverberant acoustical systems with damping The Journal of the Acoustical Society of America. 97: 687-690. DOI: 10.1121/1.412291 |
0.333 |
|
1995 |
Tang DM, Dowell EH. Damping Prediction for Stalled Rotor Flap-Lag Stability With Experimental Correlation Applied Mechanics Reviews. 48: S189-S194. DOI: 10.1115/1.3005070 |
0.401 |
|
1995 |
Tang DM, Ilgamov MA, Dowell EH. Buckling and Post-buckling Behavior of a Pipe Subjected to Internal Pressure Journal of Applied Mechanics. 62: 595-600. DOI: 10.1115/1.2895987 |
0.343 |
|
1995 |
Gottwald JA, Virgin LN, Dowell EH. Routes to escape from an energy well Journal of Sound and Vibration. 187: 133-144. DOI: 10.1006/Jsvi.1995.0506 |
0.334 |
|
1994 |
KATZ AL, DOWELL EH. FROM SINGLE WELL CHAOS TO CROSS WELL CHAOS: A DETAILED EXPLANATION IN TERMS OF MANIFOLD INTERSECTIONS International Journal of Bifurcation and Chaos. 4: 933-941. DOI: 10.1142/S0218127494000666 |
0.36 |
|
1994 |
Lyle KH, Dowell EH. Acoustic radiation damping of flat rectangular plates subjected to subsonic flows. Part I: Isotropic Journal of Fluids and Structures. 8: 711-735. DOI: 10.1016/S0889-9746(94)90180-5 |
0.386 |
|
1994 |
Dowell EH, Murphy KD, Katz AL. Simplified predictive criteria for the onset of chaos Nonlinear Dynamics. 6: 247-263. DOI: 10.1007/Bf00053385 |
0.317 |
|
1994 |
Ilgamov M, Tang D, Dowell E. Flutter and Forced Response of a Cantilevered Pipe: The Influence of Internal Pressure and Nozzle Discharge Journal of Fluids and Structures. 8: 139-156. DOI: 10.1006/Jfls.1994.1007 |
0.357 |
|
1993 |
Tang DM, Dowell EH. Experimental and theoretical study for nonlinear aeroelastic behavior of a flexible rotor blade Aiaa Journal. 31: 1133-1142. DOI: 10.2514/3.11738 |
0.431 |
|
1993 |
Tang DM, Dowell EH. Theoretical and Experimental Study on Nonlinear Response of a Rotor Blade to a Gust Applied Mechanics Reviews. 46: S3-S11. DOI: 10.1115/1.3122655 |
0.442 |
|
1993 |
Tang D, Dowell E. Nonlinear aeroelasticity in rotorcraft Mathematical and Computer Modelling. 18: 157-184. DOI: 10.1016/0895-7177(93)90110-K |
0.422 |
|
1993 |
Reynolds RR, Virgin LN, Dowell EH. High-dimensional chaos can lead to weak turbulence Nonlinear Dynamics. 4: 531-546. DOI: 10.1007/Bf00162231 |
0.364 |
|
1993 |
Tang D, Dowell E. Comparison of Theory and Experiment for Non-Linear Flutter and Stall Response of a Helicopter Blade Journal of Sound and Vibration. 165: 251-276. DOI: 10.1006/Jsvi.1993.1256 |
0.387 |
|
1993 |
Mahajan A, Kaza K, Dowell E. Semi-Empirical Model for Prediction of Unsteady Forces on an Airfoil with Application to Flutter Journal of Fluids and Structures. 7: 87-103. DOI: 10.1006/Jfls.1993.1007 |
0.432 |
|
1992 |
Tang DM, Dowell EH. Flutter and stall response of a helicopter blade with structural nonlinearity Journal of Aircraft. 29: 953-960. DOI: 10.2514/3.46268 |
0.409 |
|
1992 |
Peretti LF, Dowell EH. Study of intensification zones in a rectangular acoustic cavity Aiaa Journal. 30: 1199-1206. DOI: 10.2514/3.11051 |
0.338 |
|
1992 |
Peretti LF, Dowell EH. Asymptotic modal analysis of a rectangular acoustic cavity excited by wall vibration Aiaa Journal. 30: 1191-1198. DOI: 10.2514/3.11050 |
0.375 |
|
1992 |
Higuchi K, Dowell EH. Effect of structural damping on flutter of plates with a follower force Aiaa Journal. 30: 820-825. DOI: 10.2514/3.10990 |
0.354 |
|
1992 |
Kubota Y, Dowell EH. Asymptotic modal analysis for sound fields of a reverberant chamber The Journal of the Acoustical Society of America. 92: 1106-1112. DOI: 10.1121/1.404038 |
0.303 |
|
1992 |
Peretti LF, Dowell EH. Experimental Verification of the Asymptotic Modal Analysis Method as Applied to a Rectangular Acoustic Cavity Excited by Structural Vibration Journal of Vibration and Acoustics. 114: 546-554. DOI: 10.1115/1.2930297 |
0.361 |
|
1992 |
Tang D, Dowell E. Chaotic stall response of helicopter rotor in forward flight Journal of Fluids and Structures. 6: 311-335. DOI: 10.1016/0889-9746(92)90012-R |
0.404 |
|
1992 |
Gottwald JA, Virgin LN, Dowell EH. Experimental mimicry of Duffing's equation Journal of Sound and Vibration. 158: 447-467. DOI: 10.1016/0022-460X(92)90419-X |
0.405 |
|
1991 |
Weiliang Y, Dowell E. Limit cycle oscillation of a fluttering cantilever plate Aiaa Journal. 29: 1929-1936. DOI: 10.2514/3.10821 |
0.394 |
|
1991 |
Mahajan AJ, Dowell EH, Bliss DB. Role of artificial viscosity in Euler and Navier-Stokes solvers Aiaa Journal. 29: 555-559. DOI: 10.2514/3.10619 |
0.379 |
|
1991 |
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. 97: 398-413. DOI: 10.1016/0021-9991(91)90207-2 |
0.377 |
|
1991 |
Higuchi K, Dowell EH. Effect of constant transverse force on chaotic oscillations of sinusoidally excited buckled beam International Journal of Non-Linear Mechanics. 26: 419-426. DOI: 10.1016/0020-7462(91)90071-Z |
0.404 |
|
1990 |
Higuchi K, Dowell EH. Dynamic stability of a rectangular plate with four free edges subjected to a follower force Aiaa Journal. 28: 1300-1305. DOI: 10.2514/3.25208 |
0.317 |
|
1990 |
Dowell EH, Katz AL, Goldman RL. Static subsonic aeroelastic stability of a shell wrapped around a rigid surface Aiaa Journal. 28: 732-739. DOI: 10.2514/3.10453 |
0.395 |
|
1990 |
Dowell EH. Asymptotic modal analysis and coupled component systems The Journal of the Acoustical Society of America. 87: S91-S92. DOI: 10.1121/1.2028424 |
0.347 |
|
1989 |
Miyazawa Y, Dowell EH. Approach to modeling and estimation for uncertain systems Journal of Guidance Control and Dynamics. 12: 672-680. DOI: 10.2514/3.20461 |
0.339 |
|
1989 |
Peretti LF, Dowell EH. Bandwidth and absorption effects on intensification in a structural‐acoustic enclosure The Journal of the Acoustical Society of America. 86: S21-S21. DOI: 10.1121/1.2027415 |
0.333 |
|
1989 |
Higuchi K, Dowell E. Dynamic stability of a completely free plate subjected to a controlled non-conservative follower force Journal of Sound and Vibration. 132: 115-128. DOI: 10.1016/0022-460X(89)90875-4 |
0.33 |
|
1989 |
Higuchi K, Dowell E. 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. 129: 255-269. DOI: 10.1016/0022-460X(89)90581-6 |
0.357 |
|
1989 |
Pezeshki C, Dowell EH. Generation and analysis of Lyapunov exponents for the buckled beam International Journal of Non-Linear Mechanics. 24: 79-97. DOI: 10.1016/0020-7462(89)90001-2 |
0.755 |
|
1988 |
Miyazawa Y, Dowell EH. Principal coordinate realization of state estimation and its application of order reduction Journal of Guidance Control and Dynamics. 11: 286-288. DOI: 10.2514/3.20308 |
0.31 |
|
1988 |
Dowell EH. Unsteady Transonic Aerodynamics and Aeroelasticity Applied Mechanics Reviews. 41: 299-319. DOI: 10.2322/Jjsass1969.33.679 |
0.463 |
|
1988 |
Kubota Y, Dionne HD, Dowell EH. Asymptotic Modal Analysis and Statistical Energy Analysis of an Acoustic Cavity Journal of Vibration and Acoustics. 110: 371-376. DOI: 10.1115/1.3269528 |
0.344 |
|
1988 |
Moon FC, Dowell E, Pezeshki C. Chaotic Vibrations: An Introduction for Applied Scientists and Engineers Journal of Applied Mechanics. 55: 997-998. DOI: 10.1115/1.3173762 |
0.734 |
|
1988 |
Tang DM, Dowell EH. On the Threshold Force for Chaotic Motions for a Forced Buckled Beam Journal of Applied Mechanics. 55: 190-196. DOI: 10.1115/1.3173628 |
0.343 |
|
1988 |
Tang D, Dowell E. Chaotic oscillations of a cantilevered pipe conveying fluid Journal of Fluids and Structures. 2: 263-283. DOI: 10.1016/S0889-9746(88)80011-2 |
0.352 |
|
1988 |
Ferri A, Dowell E. Frequency domain solutions to multi-degree-of-freedom, dry friction damped systems Journal of Sound and Vibration. 124: 207-224. DOI: 10.1016/S0022-460X(88)80183-4 |
0.356 |
|
1988 |
Dowell E, Pezeshki C. On necessary and sufficient conditions for chaos to occur in Duffing's equation: an Heuristic approach Journal of Sound and Vibration. 121: 195-200. DOI: 10.1016/S0022-460X(88)80023-3 |
0.756 |
|
1988 |
Pezeshki C, Dowell E. On Chaos and fractal behavior in a generalized duffing's system Physica D: Nonlinear Phenomena. 32: 194-209. DOI: 10.1016/0167-2789(88)90051-6 |
0.74 |
|
1987 |
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. 32: 45-53. DOI: 10.4050/Jahs.32.1.45 |
0.331 |
|
1987 |
Pierre C, Tang DM, Dowell EH. Localized vibrations of disordered multispan beams - Theory and experiment Aiaa Journal. 25: 1249-1257. DOI: 10.2514/3.9774 |
0.557 |
|
1987 |
Tang DM, Dowell EH, Albright JE. Damping in beams with multiple dry friction supports Journal of Aircraft. 24: 820-832. DOI: 10.2514/3.45526 |
0.359 |
|
1987 |
Pierre C, Dowell E. Localization of vibrations by structural irregularity Journal of Sound and Vibration. 114: 549-564. DOI: 10.1016/S0022-460X(87)80023-8 |
0.568 |
|
1987 |
Pezeshki C, Dowell E. An examination of initial condition maps for the sinusoidally excited buckled beam modeled by the Duffing's equation Journal of Sound and Vibration. 117: 219-232. DOI: 10.1016/0022-460X(87)90535-9 |
0.769 |
|
1987 |
Fang T, Dowell EH. Numerical simulations of periodic and chaotic responses in a stable duffing system International Journal of Non-Linear Mechanics. 22: 401-425. DOI: 10.1016/0020-7462(87)90033-3 |
0.322 |
|
1986 |
Tang DM, Dowell EH. Random response of beams and plates with slipping at support boundaries Aiaa Journal. 24: 1354-1361. DOI: 10.2514/3.9443 |
0.371 |
|
1986 |
Tang D, Dowell E. Influence of nonlinear blade damping on helicopter ground resonance instability Journal of Aircraft. 23: 104-110. DOI: 10.2514/3.45275 |
0.406 |
|
1986 |
Dowell EH, Pezeshki C. On the Understanding of Chaos in Duffings Equation Including a Comparison With Experiment Journal of Applied Mechanics. 53: 5-9. DOI: 10.1115/1.3171739 |
0.765 |
|
1986 |
Tang D, Dowell E. Damping in beams and plates due to slipping at the support boundaries, part 2: Numerical and experimental study Journal of Sound and Vibration. 108: 509-522. DOI: 10.1016/S0022-460X(86)80044-X |
0.363 |
|
1986 |
Kubota Y, Dowell E. Experimental investigation of asymptotic modal analysis for a rectangular plate Journal of Sound and Vibration. 106: 203-216. DOI: 10.1016/0022-460X(86)90313-5 |
0.357 |
|
1986 |
Dowell E. Damping in beams and plates due to slipping at the support boundaries Journal of Sound and Vibration. 105: 243-253. DOI: 10.1016/0022-460X(86)90153-7 |
0.374 |
|
1985 |
Pierre C, Ferri AA, Dowell EH. Multi-Harmonic Analysis of Dry Friction Damped Systems Using an Incremental Harmonic Balance Method Journal of Applied Mechanics. 52: 958-964. DOI: 10.1115/1.3169175 |
0.548 |
|
1985 |
Dowell EH, Kubota Y. Asymptotic Modal Analysis and Statistical Energy Analysis of Dynamical Systems Journal of Applied Mechanics. 52: 949-957. DOI: 10.1115/1.3169174 |
0.336 |
|
1985 |
Pierre C, Dowell EH. A Study of Dynamic Instability of Plates by an Extended Incremental Harmonic Balance Method Journal of Applied Mechanics. 52: 693-697. DOI: 10.1115/1.3169123 |
0.619 |
|
1985 |
Ferri A, Dowell E. 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. 101: 55-74. DOI: 10.1016/S0022-460X(85)80038-9 |
0.364 |
|
1984 |
Ueda T, Dowell EH. Doublet-Point Method for Supersonic Unsteady Lifting Surfaces. Aiaa Journal. 22: 179-186. DOI: 10.2514/3.48437 |
0.388 |
|
1984 |
Ueda T, Dowell EH. Flutter analysis using nonlinear aerodynamic forces Journal of Aircraft. 21: 101-109. DOI: 10.2514/3.48232 |
0.401 |
|
1984 |
Dowell EH. Observation and Evolution of Chaos for an Autonomous System Journal of Applied Mechanics. 51: 664-673. DOI: 10.1115/1.3167690 |
0.325 |
|
1983 |
Dowell EH, Ueda T, Goorjian PM. Transient Decay Times and Mean Values of Unsteady Oscillations in Transonic Flow Aiaa Journal. 21: 1762-1764. DOI: 10.2514/3.8325 |
0.34 |
|
1983 |
Dowell EH, Bland SR, Williams MH. Linear/nonlinear behavior in unsteady transonic aerodynamics Aiaa Journal. 21: 38-46. DOI: 10.2514/3.8025 |
0.452 |
|
1983 |
Dowell E, Schwartz H. Forced response of a cantilever beam with a dry friction damper attached, part II: Experiment Journal of Sound and Vibration. 91: 269-291. DOI: 10.1016/0022-460X(83)90902-1 |
0.306 |
|
1983 |
Dowell E, Schwartz H. Forced response of a cantilever beam with a dry friction damper attached, part I: Theory Journal of Sound and Vibration. 91: 255-267. DOI: 10.1016/0022-460X(83)90901-X |
0.354 |
|
1983 |
Cui E, Dowell E. Postbuckling behavior of rectangular orthotropic plates with two free side edges International Journal of Mechanical Sciences. 25: 429-446. DOI: 10.1016/0020-7403(83)90057-7 |
0.355 |
|
1982 |
Ueda T, Dowell EH. A new solution method for lifting surfaces in subsonic flow Aiaa Journal. 20: 348-355. DOI: 10.2514/3.7916 |
0.387 |
|
1982 |
Dowell EH. Flutter of a buckled plate as an example of chaotic motion of a deterministic autonomous system Journal of Sound and Vibration. 85: 333-344. DOI: 10.1016/0022-460X(82)90259-0 |
0.359 |
|
1982 |
Dowell EH. Component mode analysis of a simple non-linear, non-conservative system Journal of Sound and Vibration. 80: 233-246. DOI: 10.1016/0022-460X(82)90193-6 |
0.347 |
|
1981 |
Dowell EH. Crack extension in a double cantilevered beam model Journal of Applied Physics. 52: 5356-5360. DOI: 10.1063/1.329394 |
0.317 |
|
1981 |
Dowell E. Non-linear oscillator models in bluff body aero-elasticity Journal of Sound and Vibration. 75: 251-264. DOI: 10.1016/0022-460X(81)90343-6 |
0.386 |
|
1980 |
Tongue BH, Dowell EH. Component mode analysis of nonlinear, nonconservative systems Journal of Applied Mechanics. 50: 204-209. DOI: 10.1115/1.3166994 |
0.301 |
|
1980 |
Dowell E. A Simplified Theory of Oscillating Aerofoils in Transonic Flow: Review and Extension Aeronautical Quarterly. 31: 252-284. DOI: 10.1017/S0001925900008945 |
0.394 |
|
1979 |
Horikawa H, Dowell EH. An Elementary Explanation of the Flutter Mechanism with Active Feedback Controls Journal of Aircraft. 16: 225-232. DOI: 10.2514/3.58509 |
0.351 |
|
1978 |
Alexandridis AA, Dowell EH, Moon FC. The Coupled Response of a Dynamic Element Riding on a Continuously Supported Beam Journal of Applied Mechanics. 45: 864-870. DOI: 10.1115/1.3424433 |
0.36 |
|
1978 |
Dowell E. Comments on non-linear flexural vibrations of a cylindrical shell Journal of Sound and Vibration. 60: 596-597. DOI: 10.1016/S0022-460X(78)80097-2 |
0.313 |
|
1978 |
Horikawa H, Dowell EH, Moon FC. Active feedback control of a beam subjected to a nonconservative force International Journal of Solids and Structures. 14: 821-839. DOI: 10.1016/0020-7683(78)90073-2 |
0.382 |
|
1977 |
Dowell EH, Ventres CS. Flutter of an elastic plate under tension Aiaa Journal. 15: 1653-1655. DOI: 10.2514/3.7468 |
0.382 |
|
1977 |
Williams MH, Chi MR, Ventres CS, Dowell EH. Aerodynamic Effects of Inviscid Parallel Shear Flows Aiaa Journal. 15: 1159-1166. DOI: 10.2514/3.60767 |
0.394 |
|
1977 |
Vaicaitis R, Dowell E. Response of Space Shuttle Surface Insulation Panels to Acoustic Pressure Journal of Spacecraft and Rockets. 14: 739-746. DOI: 10.2514/3.57257 |
0.332 |
|
1977 |
Dowell EH. Reverberation time, absorption, and impedance The Journal of the Acoustical Society of America. 62: S41-S41. DOI: 10.1121/1.381983 |
0.323 |
|
1977 |
Dowell E, Traybar J, Hodges D. An experimental-theoretical correlation study of non-linear bending and torsion deformations of a cantilever beam Journal of Sound and Vibration. 50: 533-544. DOI: 10.1016/0022-460X(77)90501-6 |
0.33 |
|
1977 |
Dowell E, Gorman G, Smith D. Acoustoelasticity: General theory, acoustic natural modes and forced response to sinusoidal excitation, including comparisons with experiment Journal of Sound and Vibration. 52: 519-542. DOI: 10.1016/0022-460X(77)90368-6 |
0.35 |
|
1976 |
Kornecki A, Dowell E, O'Brien J. On the aeroelastic instability of two-dimensional panels in uniform incompressible flow Journal of Sound and Vibration. 47: 163-178. DOI: 10.1016/0022-460X(76)90715-X |
0.402 |
|
1975 |
McLean JD, Dowell EH. Swirling flows between coaxial cylinders with injection by radial jets Aiaa Journal. 13: 1435-1440. DOI: 10.2514/3.7012 |
0.343 |
|
1975 |
DOWELL EH. Vibration and flutter analysis of reusable surface insulation panels Journal of Spacecraft and Rockets. 12: 44-50. DOI: 10.2514/3.27805 |
0.312 |
|
1974 |
DOWELL EH, SRINIVASAN AV, McLEAN JD, AMBROSE J. Aeroelastic Stability of Cylindrical Shells Subjected to a Rotating Flow Aiaa Journal. 12: 1644-1651. DOI: 10.2514/3.49573 |
0.381 |
|
1974 |
VAICAITIS R, DOWELL E, VENTRES C. Nonlinear Panel Response by a Monte Carlo Approach Aiaa Journal. 12: 685-691. DOI: 10.2514/3.49320 |
0.37 |
|
1974 |
Yan MJ, Dowell EH. Elastic Sandwich Beam or Plate Equations Equivalent to Classical Theory Journal of Applied Mechanics. 41: 526-527. DOI: 10.1115/1.3423327 |
0.307 |
|
1974 |
Dowell E. Dynamic analysis of an elastic plate on a thin, elastic foundation Journal of Sound and Vibration. 35: 343-360. DOI: 10.1016/0022-460X(74)90065-0 |
0.348 |
|
1974 |
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. 10: 361-381. DOI: 10.1016/0020-7683(74)90083-3 |
0.369 |
|
1973 |
DOWELL EH. Theoretical Vibration and Flutter Studies of Point Supported Panels Journal of Spacecraft and Rockets. 10: 389-395. DOI: 10.2514/3.61896 |
0.368 |
|
1973 |
DOWELL EH, VENTRES CS. Derivation of Aerodynamic Kernel Functions Aiaa Journal. 11: 1586-1588. DOI: 10.2514/3.50642 |
0.402 |
|
1972 |
Yan M, Dowell EH. Governing Equations for Vibrating Constrained-Layer Damping Sandwich Plates and Beams Journal of Applied Mechanics. 39: 1041-1046. DOI: 10.1115/1.3422825 |
0.319 |
|
1972 |
Dowell EH. Free Vibrations of an Arbitrary Structure in Terms of Component Modes Journal of Applied Mechanics. 39: 727-732. DOI: 10.1115/1.3422780 |
0.301 |
|
1971 |
DOWELL EH. Generalized aerodynamic forces on a flexible plate undergoing transient motion in a shear flow with an application to panel flutter Aiaa Journal. 9: 834-841. DOI: 10.2514/3.6283 |
0.368 |
|
1971 |
Dowell EH. Free Vibrations of a Linear Structure With Arbitrary Support Conditions Journal of Applied Mechanics. 38: 595-600. DOI: 10.1115/1.3408860 |
0.333 |
|
1970 |
VENTRES CS, DOWELL EH. Comparison of theory and experiment for nonlinear flutter of loaded plates Aiaa Journal. 8: 2022-2030. DOI: 10.2514/3.6041 |
0.322 |
|
1970 |
DOWELL EH. Flutter of buckled plates at zero dynamic pressure Aiaa Journal. 8: 583-584. DOI: 10.2514/3.5717 |
0.312 |
|
1970 |
DOWELL EH. Panel flutter - A review of the aeroelastic stability of plates and shells Aiaa Journal. 8: 385-399. DOI: 10.2514/3.5680 |
0.308 |
|
1970 |
DOWELL EH. Nonlinear flutter of curved plates. II Aiaa Journal. 8: 259-261. DOI: 10.2514/3.5653 |
0.305 |
|
1970 |
Dowell E. Noise or flutter or both? Journal of Sound and Vibration. 11: 159-180. DOI: 10.1016/S0022-460X(70)80061-X |
0.36 |
|
1969 |
DOWELL EH. Nonlinear flutter of curved plates. Aiaa Journal. 7: 424-431. DOI: 10.2514/3.5124 |
0.382 |
|
1969 |
Dowell EH. Transmission of Noise from a Turbulent Boundary Layer through a Flexible Plate into a Closed Cavity The Journal of the Acoustical Society of America. 46: 238-252. DOI: 10.1121/1.1911676 |
0.402 |
|
1969 |
Dowell EH. Non-linear theory of unstable plane Poiseuille flow Journal of Fluid Mechanics. 38: 401-414. DOI: 10.1017/S0022112069000243 |
0.401 |
|
1968 |
Dowell E, Ventres C. Modal equations for the nonlinear flexural vibrations of a cylindrical shell International Journal of Solids and Structures. 4: 975-991. DOI: 10.1016/0020-7683(68)90017-6 |
0.369 |
|
1967 |
DOWELL EH. On the nonlinear flexural vibrations of rings. Aiaa Journal. 5: 1508-1509. DOI: 10.2514/3.4236 |
0.32 |
|
1967 |
Widnall SE, Dowell EH. Aerodynamic forces on an oscillating cylindrical duct with an internal flow Journal of Sound and Vibration. 6: 71-85. DOI: 10.1016/0022-460X(67)90159-9 |
0.405 |
|
1966 |
Dowell EH. Nonlinear oscillations of a fluttering plate. II. Aiaa Journal. 5: 1856-1862. DOI: 10.2514/3.4316 |
0.375 |
|
1966 |
Dowell EH. Flutter of infinitely long plates and shells. I - Plate. Aiaa Journal. 4: 1370-1377. DOI: 10.2514/3.3680 |
0.421 |
|
1966 |
DOWELL EH, WIDNALL SE. Generalized aerodynamic forces on an oscillating cylindrical shell -Subsonic and supersonic flow. Aiaa Journal. 4: 607-610. DOI: 10.2514/3.3496 |
0.363 |
|
1966 |
Dowell EH, Widnall SE. Generalized aerodynamic forces on an oscillating cylindrical shell Quarterly of Applied Mathematics. 24: 1-17. DOI: 10.1090/Qam/99934 |
0.311 |
|
1964 |
DOWELL E. Flutter of multibay panels at high supersonic speeds Aiaa Journal. 2: 1805-1814. DOI: 10.2514/3.2669 |
0.367 |
|
1964 |
VOSS HM, DOWELL EH. Effect of aerodynamic damping on flutter of thin panels Aiaa Journal. 2: 119-120. DOI: 10.2514/3.2233 |
0.335 |
|
1963 |
DUGUNDJI J, DOWELL E, PERKIN B. SUBSONIC FLUTTER OF PANELS ON CONTINUOUS ELASTIC FOUNDATIONS Aiaa Journal. 1: 1146-1154. DOI: 10.2514/3.1738 |
0.325 |
|
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