Transition measurements via heat-transfer instrumentation on a 0.5 bluntness 9.75-deg cone at Mach 7 with and without mass addition
Author:
Affiliation:
1. USAF, Arnold Engineering Development Center, Air Force Station, TN
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1985-1004
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1. Flow characteristics of porous media and surface liquid film interactions
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4. The status of research in turbulent boundary layers with fluid injection
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1. Hypersonic Boundary-Layer Transition with Ablation and Blowing;Journal of Spacecraft and Rockets;2010-03
2. Numerical Simulation of Hypersonic Boundary Layer Receptivity and Stability on Blunt Circular Cones;47th AIAA Aerospace Sciences Meeting including The New Horizons Forum and Aerospace Exposition;2009-01-05
3. Hypersonic laminar–turbulent transition on circular cones and scramjet forebodies;Progress in Aerospace Sciences;2004-02
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