Aerothermodynamic flight simulation capabilities for aerospace vehicles-Reference-Cited by-同舟云学术

Aerothermodynamic flight simulation capabilities for aerospace vehicles

Published:1998-06-15 Issue: Volume: Page:
ISSN:
Container-title:20th AIAA Advanced Measurement and Ground Testing Technology Conference
language:
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Author:

Miller Charles¹

Affiliation:

1. NASA, Langley Research Center, Hampton, VA

Publisher

American Institute of Aeronautics and Astronautics

Link

http://arc.aiaa.org/doi/pdf/10.2514/6.1998-2600

Reference57 articles.

1. 6," Journal of Spacecraft andRockets,vol.34, No. 4,July-August 1997,pp.416-425.

2. "Results of Aerothermodynamic and Boundary Layer Transition Testing of 0.0362-Scale X-38 (Rev 3.1)Vehiclein NASA Langley 20-Inch Mach 6Tunnel,"NASATM 112857,Sep.1997. Berry, S. A. Horvath, T. J., DiFulvio, M., Glass, C. E.

3. and Merski, N. R. "X-34 Experimental Aeroheating at Mach 6 and 10,"AIAA Paper 98-0881,Jan.1998. Brauckmann, Gregory J., Paulson, J. W. Jr., and

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