Publisher
American Institute of Aeronautics and Astronautics
Cited by
2 articles.
订阅此论文施引文献
订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献
1. Nonlinear Finite Element Modal Formulation for Panel Flutter with Thermal Effects and Acoustic Excitation;53rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference<BR>20th AIAA/ASME/AHS Adaptive Structures Conference<BR>14th AIAA;2012-04-23
2. Effects of oscillating shock waves on the dynamics of fluttering panels;19th AIAA Applied Aerodynamics Conference;2001-06-11