Impact of Panel Vibrations on the Dynamic Field Properties in Supersonic flow
Author:
Affiliation:
1. North Carolina State University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2021-2926
Reference23 articles.
1. Aeroelasticity of Plates and Shells
2. On the interaction of an oblique shock with a flexible panel
3. A. Gogulapati, R. Deshmukh, A. R. Crowell, J. J. McNamara, V. Vyas, X.Q. Wang, M. Mignolet, T. Beberniss, S. M. Spottswood, T. G. Eason, “Response of a Panel to Shock Impingement: Modeling and Comparison with Experiments”, AIAA SciTech 2014-0148
4. A. Gogulapati, R. Deshmukh, A. R. Crowell, J. J. McNamara, V. Vyas, X.Q. Wang, M. Mignolet, T. Beberniss, S. M. Spottswood, T. G. Eason, “Response of a Panel to Shock Impingement: Modeling and Comparison with Experiments-Part 2”, AIAA SciTech 2015-0685
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