Fluid-Structure Interactions on a Slender Cone under Quiet Flow Conditions at Mach 6
Author:
Affiliation:
1. Sandia National Laboratories
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2017-0402
Reference20 articles.
1. 1Casper, K., Pressure Fluctuations Beneath Turbulent Spots and Instability Wave Packets in a Hypersonic Boundary Layer, Ph.D. Thesis,Purdue University School of Aeronautics & Astronautics, August 2012.
2. Pressure fluctuations beneath instability wavepackets and turbulent spots in a hypersonic boundary layer
3. Hypersonic Wind-Tunnel Measurements of Boundary-Layer Transition on a Slender Cone
4. Fluid Structure Interaction on a Generic Body-Flap Model in Hypersonic Flow
5. Fluid-Structure Interactions using Controlled Disturbances on a Slender Cone at Mach 8
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