Evaluation of PNS-computed heating and hypersonic shock tunnel data on sharp and inclined blunt cones
Author:
Affiliation:
1. Sandia National Laboratories, Albuquerque, NM
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1989-310
Reference17 articles.
1. Stalnaker, J. F., Nicholson, L. A, Hanline, D. S., and McGraw, E. H. "Improvements to the AFWAL Parabolized Navier-Stokes Code Formulation," Air Force Wright Aeronautical Laboratories Report AFWAL-TR86-3076, September 1986.
2. NASA Ames Research Center's parabolized Navier-Stokes code - A critical evaluation of heat-transfer predictions
Cited by 3 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. Numerical study of turbulent flow of partly ionized air in a viscous shock layer;Journal of Applied Mechanics and Technical Physics;1994-09
2. Joint computational/experimental aerodynamics research on hypersonicvehicle. II - Computational results;AIAA Journal;1992-08
3. Joint computational experimental aerodynamics research on a hypersonic vehicle. II - Computational results;29th Aerospace Sciences Meeting;1991-01-07
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