Experimental Studies in Hypersonic Flows for Facility and Code Validation
Author:
Affiliation:
1. Calspan-University of Buffalo Research Center
2. Redstone Arsenal
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1304
Reference13 articles.
1. Experimental Studies to Examine Viscous/Inviscid Interactions and Flow Chemistry Effects of Hypersonic Vehicle Performance
2. Shock interaction phenomena in hypersonic flows
3. Database of Aerothermal Measurements in Hypersonic Flow "Building Block" Experiments
4. Shock wave-turbulent boundary layer interaction in hypersonic flow
Cited by 3 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Experimental investigation of axisymmetric hypersonic shock-wave/turbulent-boundary-layer interactions;Journal of Fluid Mechanics;2013-01-02
2. Reviews of Studies of Boundary Layer Transition in Hypersonic Flows Over Axisymmetric and Elliptic Cones Conducted in the CUBRC Shock Tunnels;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
3. Analysis and Ground Test of Aerothermal Effects on Spherical Capsule Geometries;38th Fluid Dynamics Conference and Exhibit;2008-06-15
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