Computation of nonequilibrium merged stagnation shock layers by successive accelerated replacement-Reference-Cited by-同舟云学术

Computation of nonequilibrium merged stagnation shock layers by successive accelerated replacement

Published:1971-02 Issue:2 Volume:9 Page:262-269
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

DELLINGER THOMAS C.¹

Affiliation:

1. General Electric Company, Philadelphia, Pa.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.6161

Reference17 articles.

1. Viscous Aerodynamic Characteristics in Hypersonic Rarefied Gas Flow

2. Ho, H. T. and Probstein, R. F. "The Compressible Viscous Layer in Rarefied Hypersonic Flow/' Rarefied Gas Dynamics, edited by L. Talbot, Academic Press, New York, 1961, pp.525-552.

3. RAREFIED HYPERSONIC FLOW OVER A SPHERE

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