X-38 experimental aeroheating at Mach 10
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2001-2828
Reference51 articles.
1. Barret C. 1999.Lifting Body Stability and Control NASA TM-1999-209255
2. Berry SA, Horvath TJ, Roback VE, Williams GB. 1997. Results of Aerothermodynamic and Boundary-Layer Transition Testing of 0.0362-Scale X-38(Rev.3.1) Vehicle in NASA Langley 20-Inch Mach 6 Tunnel NASA TM-112857.
3. Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness
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