Prediction of nonlinear panel response using proper orthogonal decomposition

Author:

Beran Philip1,Pettit Chris1

Affiliation:

1. USAF, Research Lab., Wright-Patterson AFB, OH

Publisher

American Institute of Aeronautics and Astronautics

Cited by 19 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

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3. A Method to Compute Flameout Limits of Scramjet-Powered Hypersonic Vehicles;51st AIAA/SAE/ASEE Joint Propulsion Conference;2015-07-23

4. Nonlinear plate aeroelastic response with uncertain stiffness and boundary conditions;Structure and Infrastructure Engineering;2006-09

5. Reduced-order fluid/structure modeling of a complete aircraft configuration;Computer Methods in Applied Mechanics and Engineering;2006-08

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