Response of a Thin Panel to Aerothermal Loading at Mach 6
Author:
Affiliation:
1. ARCTOS Technology Solutions, LLC, Dayton, Ohio 45432
2. Air Force Research Laboratory, Wright–Patterson Air Force Base, Ohio 45433
3. Ehrhardt Engineering, LLC, Monticello, Illinois 61856
Funder
Air Force Office of Scientific Research
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.J060404
Reference14 articles.
1. Hypersonic Fluid–Structure Interactions Due to Intermittent Turbulent Spots on a Slender Cone
2. Exploring the response of a thin, flexible panel to shock-turbulent boundary-layer interactions
3. Experiments on the Interaction of a Fast-Moving Shock with an Elastic Panel
4. RobbinsB.CasperK.CoffinP.MeshM.FieldR. Jr. “Quantifying the Structural Response of a Slender Cone to Turbulent Spots at Mach 6,” AIAA Paper 2019-1631, Jan. 2019. 10.2514/6.2019-1631
5. GogulapatiA.DeshmukhR.McNamaraJ.VyasV.WangX.MignoletM.BebernissT.SpottswoodS.EasonT. “Response of a Panel to Shock Impingement: Modeling and Comparison with Experiments—Part 2,” AIAA Paper 2015-0685, Jan. 2015. 10.2514/6.2015-0685
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