Full-field, dynamic pressure and displacement measurements of a panel excited by shock boundary-layer interaction

Author:

Spottswood Stephen M.1,Eason Thomas1,Beberniss Timothy1

Affiliation:

1. Air Force Research Laboratory

Publisher

American Institute of Aeronautics and Astronautics

Reference29 articles.

1. R.Quiroz,J.Embler,R.Jacobs,G. Tzong,andS.Liguore,"PredictiveCapabilityforHypersonicStructural Response and Life Prediction: Phase II - Detailed Designof Hypersonic Cruise Vehicle Hot-Structure ," Technical Report, AFRL-RQ-WP-TR-2012-0265,February2012.

2. B.Zuchowski,"PredictiveCapabilityforHypersonicStructuralResponseandLifePrediction:PhaseII-Detailed DesignofHypersonic Cruise Vehicle Hot-Structure," Technical Report, AFRL-RB-WP-TR-2012-0280, May2012.

3. Acoustic testing of high-temperature panels

4. The impact of flow induced loads on snap-through behavior of acoustically excited, thermally buckled panels

5. Thermoacoustic loads and fatigue of hypersonic vehicle skin panels

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