Analysis of nonlinear aeroelastic response of curved panels under shock impingements
Author:
Funder
National Natural Science Foundation of China
Aeronautical Science Foundation of China
Publisher
Elsevier BV
Subject
Mechanical Engineering
Reference26 articles.
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3. Numerical simulation of nonlinear aeroelastic behaviors of composite panels in transonic flow;An;J. Sound Vib.,2020
4. Azzouz, M., Mei, C., 2005. Nonlinear flutter of cylindrical panels under yawed supersonic flow using finite elements. In: 46th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics & Materials Confer.
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