Comparisons of CFD flow field solutions with experimental data at Mach 14
Author:
Affiliation:
1. Sandia National Laboratories, Albuquerque, NM
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1986-742
Reference13 articles.
1. of Attack," AIAA-81-0050, 1981.
2. Maydew, R. C. "Sandia Laboratory Aerodynamic Test Facilities,"Sandia National Laboratories Report SC-4937(M), September 1963.
3. Peterson, C. W., Reed, J. F., and Curry, W. H. "Electric Heater Development for A High Performance Mach Number 14 Wind Tunnel,"AIAA-74-616, July 1974.
4. Evaluation of inviscid/boundary layer and parabolized Navier-Stokes solutions for design of reentry vehicles
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