Shock Wave Structure in a Rarefied Hypersonic Flow on Power Law Shaped Leading Edges
Author:
Affiliation:
1. Instituto Nacional de Pesquisas Espaciais
2. University of Maryland
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-1134
Reference18 articles.
1. 1Van Dyke, M. D. "A study of Hypersonic Small-Disturbance Theory", NACA TN-3173,1954.
2. Inviscid Hypersonic Flow Over Blunt-Nosed Slender Bodies
3. An experimental investigation of asymptotic hypersonic flows
4. Shock-wave shapes on hypersonic axisymmetric power-law bodies
5. Some aspects of hypersonic flow over power law bodies
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1. Influence of Gas-Surface Interaction on Hypersonic Aerothermodynamic Performance of Flat-Nose Power-Law Bodies;44th AIAA Aerospace Sciences Meeting and Exhibit;2006-01-09
2. Aerothermodynamic Performance Analysis of Hypersonic Flow on Power Law Leading Edges;Journal of Spacecraft and Rockets;2005-07
3. Structure of the Shock Wave on Flat-Nose Power-Law Bodies;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10
4. Some Extentions to the Aerothermodynamic Performance Study of Flat-Nose Power-Law Bodies;43rd AIAA Aerospace Sciences Meeting and Exhibit;2005-01-10
5. Aerothermodynamic Characteristics of Flat-Nose Power-Law Bodies in Low-Density Hypersonic Flow;22nd Applied Aerodynamics Conference and Exhibit;2004-06-20
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