Magnetohydrodynamic hypersonic viscous flow past a blunt body
Author:
Affiliation:
1. The Rand Corporation, Santa Monica, Calif
2. Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.2465
Reference5 articles.
1. Rosser, J B , Newton, R R , and Gross G L , Mathematical Theory of Rocket Flight (McGraw-Hill Book Co , Inc , New York 1947) p20
2. November 1958;Bush W B
3. Hypersonic Viscous Flow Near the Stagnation Point in the Presence of Magnetic Field
4. Bellman, R Kagiwada, H , and Kalaba, R E"Orbit determination as a multi-point boundary value problem and quasilinearization, ' Proc Natl Acad Sci 48,1327-1329(1962)
5. Bush W B , "A note on magnetohydrodynamic hypersonic flow past a blunt body ' J Aerospace Sci 26, 536-537 (1959)
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