Results of an industry representative study of code to code validation of axisymmetric configurations at hypervelocity flight conditions
Author:
Affiliation:
1. USAF, Flight Dynamics Laboratory, Wright-Patterson AFB, OH
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1988-2691
Reference12 articles.
1. Newnn. R.D. and Patterson, J.L. "Resuits of an Industry Representative Study of Code-to-Code Validation of Axisynnetric Configurations at Hypervelocity Flight Conditions", AFYAL TR to be pub 1 ished
2. Chaussee. D.S. "NASA h e 5 Research Center's Paratoifzed Navier-Stokes Code: A Critical Evaluation of Heat Transfer Predictions". AIAA Paper 87-1474. June 1987
Cited by 2 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Prediction of supersonic/hypersonic viscous flows over re-entry vehicles and decoys;Journal of Spacecraft and Rockets;1990-09
2. Parabolized Navier-Stokes predictions of three-dimensional hypersonic flows with strong crossflow effects;Journal of Thermophysics and Heat Transfer;1990-01
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