Response of a Panel to Shock Impingement: Modeling and Comparison with Experiments - Part 2
Author:
Affiliation:
1. Ohio State University
2. Arizona State University
3. Air Force Research Laboratory
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2015-0685
Reference32 articles.
1. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels
2. Full-field, dynamic pressure and displacement measurements of a panel excited by shock boundary-layer interaction
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