Flutter/Aeroelastic Response of Panels via a Combined Galerkin-Volterra Series Approach

Author:

Marzocca Piergiovanni,Lazzaro Riccardo,Librescu Liviu

Publisher

American Institute of Aeronautics and Astronautics

Reference12 articles.

1. Librescu, L., Elastostatics and Kinetics of Anisotropic and Heterogeneous Shell-Type Structures, Chapter 1: Aeroelastic Stability of Anisotropic Multilayered Thin Panels,1st ed., Book series: Mechanics of Elastic Stability, edited by H. Leipholz,Noordhoff International Publishing, Leyden, The Netherlands,1975, pp.53-63, 106-158, Appendix A, pp. 543-550.

2. Supersonic/Hypersonic Flutter and Postflutter of Geometrically Imperfect Circular Cylindrical Panels

3. Aeroelastic response of nonlinear wing sections using a functional series technique

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1. Volterra-series-based nonlinear system modeling and its engineering applications: A state-of-the-art review;Mechanical Systems and Signal Processing;2017-03

2. Piecewise Global Volterra Nonlinear Modeling and Characterization for Aircraft Dynamics;Journal of Guidance, Control, and Dynamics;2009-05

3. Effects of Proper Orthogonal Decomposition on Identification Using the Minimum Model Error Algorithm;47th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference<BR> 14th AIAA/ASME/AHS Adaptive Structures Conference<BR> 7th;2006-05

4. Panel Flutter Model Identification Using the Minimum Model Error Method on the Forced Response Measurements;Journal of Vibration and Acoustics;2006-02-08

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