Shock wave shapes on a sharp flat plate in rarefied hypersonic flow.-Reference-Cited by-同舟云学术

Shock wave shapes on a sharp flat plate in rarefied hypersonic flow.

Published:1966-01 Issue:1 Volume:4 Page:184-186
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

McCROSKEY W. J.¹,McDOUGALL J. G.¹

Affiliation:

1. Princeton University, Princeton, N. J.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.3417

Reference12 articles.

1. Hayes, W. D. and Probstein, R. F., Hypersonic Flow Theory (Academic Press Inc., New York,1959), pp.333-389.

2. Hypersonic Flow Near the Leading Edge of a Flat Plate

3. Oguchi, H. "The sharp leading edge problem in hypersonic flow/' Rarefied Gas Dynamics (Academic Press Inc., New York,1961), suppl. 1, pp.501-524.

4. Probstein, R. F. and Pan, Y. S. "Shock structure and the leading edge problem," Rarefied Gas Dynamics (Academic Press Inc., New York,1963), suppl. 2, Vol.II, pp.192-211.

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