Return to Flight Testing of a 3.5% Scale Space Shuttle OTS and OT Model at Mach Numbers of 3.5 and 4.0
Author:
Affiliation:
1. CUBRC
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-720
Reference14 articles.
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3. AIAA Journal. Vol 32,no8. Pgs 1598-1605. August 1994.
4. Brown, James. "Turbulence Model Validationfor Hypersonic Flows". AIAA Paper 2002-3308. 8TH
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