Power law shaped leading edges in rarefied hypersonic flow
Author:
Affiliation:
1. National Inst. for Space Research, Sao Paulo, Brazil
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-645
Reference21 articles.
1. *Van Dyke, M. D. "A study of Hypersonic Small-Disturbance Theory",NACA TN-3173, 1954.
2. On the Hypersonic Viscous Flow Past Slender Bodies of Revolution
3. 3Lees, L. and Kubota, T. "Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies/' J. of the AeronauticalSciences,vol.24 , 1957,pp.195-202.
4. Hypersonic Flow over Slender Bodies Associated with Power-Law Shocks
5. An experimental investigation of asymptotic hypersonic flows
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. Direct Simulation of Ionization Around Power-Law Leading Edges in Rarefied Hypersonic Flow;34th AIAA Plasmadynamics and Lasers Conference;2003-06-23
2. Shock Wave Structure in a Rarefied Hypersonic Flow on Power Law Shaped Leading Edges;41st Aerospace Sciences Meeting and Exhibit;2003-01-06
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