CEAS/AIAA/ICASE/NASA Langley International Forum on Aeroelasticity and Structural Dynamics 1999. Pt. 1

The proceedings of a workshop sponsored by the Confederation of European Aerospace Societies (CEAS), the American Institute of Aeronautics and Astronautics (AIAA), the National Aeronautics and Space Administration (NASA), Washington, D.C., and the Institute for Computer Applications in Science and Engineering (ICASE), Hampton, Virginia, and held in Williamsburg, Virginia June 22-25, 1999 represent a collection of the latest advances in aeroelasticity and structural dynamics from the world community. Research in the areas of unsteady aerodynamics and aeroelasticity, structural modeling and optimization, active control and adaptive structures, landing dynamics, certification and qualification, and validation testing are highlighted in the collection of papers. The wide range of results will lead to advances in the prediction and control of the structural response of aircraft and spacecraft.

[1]  T. Y. Yang,et al.  Nonlinear panel flutter using high-order triangular finite elements , 1983 .

[2]  David Y. Xue,et al.  Finite element nonlinear panel flutter with arbitrary temperatures in supersonic flow , 1992 .

[3]  Earl H. Dowell,et al.  Limit cycle oscillation of a fluttering cantilever plate , 1991 .

[4]  Earl H. Dowell,et al.  Flutter of a buckled plate as an example of chaotic motion of a deterministic autonomous system , 1982 .

[5]  P. Mantegazza,et al.  Multi-Input/Multi-Output Adaptive Active Flutter Suppression for a Wing Model , 1998 .

[6]  R. Vaicaitis,et al.  NONLINEAR RESPONSE OF COMPOSITE PANELS TO RANDOM EXCITATION , 1993 .

[7]  S. C. Mcintosh,et al.  Theoretical considerations of some nonlinear aspects of hypersonic panel flutter , 1974 .

[8]  F F Rudder,et al.  Sonic Fatigue Design Guide for Military Aircraft , 1975 .

[9]  N. K. Chandiramani,et al.  Nonperiodic flutter of a buckled composite panel , 1995 .

[10]  Chuh Mei,et al.  Review of Nonlinear Panel Flutter at Supersonic and Hypersonic Speeds , 1999 .

[11]  Henry T. Y. Yang,et al.  Reliability and nonlinear supersonic flutter of uncertain laminated plates , 1993 .

[12]  Earl H. Dowell,et al.  Nonlinear flutter of curved plates. , 1969 .

[13]  Robert G. Loewy,et al.  Helicopter Vibrations: A Technological Perspective , 1984 .

[14]  Chuh Mei,et al.  A Finite-Element Approach for Nonlinear Panel Flutter , 1977 .

[15]  L. Morino A perturbation method for treating nonlinear panel flutter problems. , 1969 .

[16]  B. L. Clarkso Review of Sonic Fatigue Technology , 2022 .

[17]  T. K. Varadan,et al.  Nonlinear panel flutter by finite-element method , 1988 .

[18]  H. Saunders,et al.  Random Vibration of Elastic Systems , 1987 .

[19]  G. Venkateswara Rao,et al.  Large amplitude supersonic flutter of panels with ends elastically restrained against rotation , 1980 .

[20]  Rock R. Arnold,et al.  Nonlinear Response and Fatigue of Surface Panels by the Time Domain Monte Carlo Approach , 1992 .

[21]  Chuh Mei,et al.  Finite element analysis of large-amplitude panel flutter of thin laminates , 1993 .

[22]  D. G. Liaw Nonlinear supersonic flutter of laminated composite plates under thermal loads , 1997 .

[23]  Holt Ashley,et al.  Piston Theory-A New Aerodynamic Tool for the Aeroelastician , 1956 .

[24]  V. V. Bolotin,et al.  Nonconservative problems of the theory of elastic stability , 1963 .

[25]  T. Y. Yang,et al.  Flutter of thermally buckled finite element panels , 1976 .

[26]  S. Durvasula,et al.  Flutter of simply supported, parallelogrammic, flat panels in supersonic flow. , 1966 .

[27]  Jen-Kuang Huang,et al.  Suppression of nonlinear panel flutter with piezoelectric actuators using finite element method , 1995 .

[28]  Juang Jer-Nan,et al.  State-Space System Realization With Input- and Output-Data Correlation , 1997 .

[29]  Y. C. Fung,et al.  On Two-Dimensional Panel Flutter , 1958 .

[30]  E. Laitone,et al.  Elements of Gasdynamics. , 1957 .

[31]  E. Dowell,et al.  Aeroelasticity of Plates and Shells , 1974 .

[32]  C. Mei,et al.  Nonlinear panel flutter - A finite-element approach , 1977 .

[33]  Ming-Tsang Ho,et al.  Wind tunnel testing of panel flutter control using piezoelectric actuation and iterative gain tuning , 1997, Smart Structures.

[34]  J. L. Rogers,et al.  Application of NASTRAN to large deflection supersonic flutter of panels , 1976 .

[35]  Liviu Librescu,et al.  Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures , 1975 .

[36]  David Y. Xue,et al.  Finite element frequency domain solution of nonlinear panel flutter with temperature effects and fatigue life analysis , 1991 .

[37]  Carl Gray,et al.  A finite-element method for large-amplitude, two-dimensional panel flutter at hypersonic speeds , 1989 .

[38]  E. Dowell Panel flutter - A review of the aeroelastic stability of plates and shells , 1970 .

[39]  R. Ibrahim,et al.  Nonlinear flutter of orthotropic composite panel under aerodynamic heating , 1992 .

[40]  Earl H. Dowell,et al.  Comparison of theory and experiment for nonlinear flutter of loaded plates , 1970 .

[41]  Luigi Morino,et al.  Stability Analysis of Nonlinear Differential Autonomous Systems with Applications to Flutter , 1976 .

[42]  Chuh Mei,et al.  Finite Element Nonlinear Random Response of Composite Panels of Arbitrary Shape to Acoustic and Thermal Loads , 1995 .

[43]  Robert M. Laurenson,et al.  Design Procedures for Flutter-Free Surface Panels , 1979 .

[44]  Chuh Mei,et al.  Large-amplitude finite element flutter analysis of composite panels in hypersonic flow , 1992 .

[45]  Maher N. Bismarck-Nasr,et al.  Finite Element Analysis of Aeroelasticity of Plates and Shells , 1992 .

[46]  T. Hughes,et al.  A three-node mindlin plate element with improved transverse shear , 1985 .

[47]  Victor Giurgiutiu,et al.  Engineering Feasibility of Induced Strain Actuators for Rotor Blade Active Vibration Control , 1994, Smart Structures.

[48]  Paolo Mantegazza,et al.  Multi-Body Aeroelastic Analysis of Smart Rotor Blades, Actuated by Means of Piezo-Electric Devices , 1997 .

[49]  Norman D. Ham,et al.  Helicopter individual-blade-control research at MIT 1977-1985 , 1986 .

[50]  R. Ibrahim,et al.  Stochastic non-linear flutter of a panel subjected to random in-plane forces , 1991 .