Discrete Roughness Transition for Hypersonic Flight Vehicles
Author:
Affiliation:
1. NASA Langley Research Center
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-307
Reference41 articles.
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2. Campbell,C.,Anderson, B., Bourland,G.,Bouslog,S.,Cassady, A.,Horvath, T., Berry,S., Gnoffo,P.,Wood,B., Reuther, J.,Driver, D.,Chao, D., and Picetti,D. "Orbiter Return To FlightEntry Aeroheating," AIAA-2006-2917, June2006.
3. Comments on Hypersonic Boundary-Layer Transition
4. Williamson,W.E. "HypersonicFlightTesting,"AIAA Paper 92-3989,1992.
5. Review and Synthesis of Roughness-Dominated Transition Correlations for Reentry Applications
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