Inverse solution of blunt-body flowfields at large angle of attack.
Author:
Affiliation:
1. North American Aviation Inc., Downey, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.4140
Reference17 articles.
1. May 1964;Waldman G.
2. July 1964;Lomax H.
Cited by 6 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. Trajectory based, 3-dimensional heating and ablation calculations for the Apollo Lunar/Earth return capsule;28th Thermophysics Conference;1993-07-06
2. A Blunt Body in a Supersonic Stream;Annual Review of Fluid Mechanics;1976-01
3. Entropy Layer on a Supersonic Plane Flat Nose at Incidence;AIAA Journal;1975-02
4. Time-Split Finite-Volume Method for Three-Dimensional Blunt-Body Flow;AIAA Journal;1973-11
5. The value of the entropy at the surface of paraboloids;Fluid Dynamics;1972
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