An engineering aerodynamic heating method for hypersonic flow
Author:
Affiliation:
1. NASA, Langley Research Center, Hampton, VA
2. North Carolina State University, Raleigh
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1992-499
Reference10 articles.
1. Gnoffo, P. A. "An Upwind-Biased, Point-Implicit TP-3018, Aug. 1990. Relaxation Algorithm for Viscous, Compressible Perfect-Gas Flows,"NASA TP-2953, Feb. 1990. tric Hypersonic Flow,"
2. Comparisons of STS-1 experimental and predicted heating rates
3. Analysis of STS-2 experimental heating rates and transition data
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