Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt Bodies-Reference-Cited by-同舟云学术

Hypersonic Three-Dimensional Viscous Shock-Layer Flows over Blunt Bodies

Published:1978-12 Issue:12 Volume:16 Page:1279-1286
ISSN:0001-1452
Container-title:AIAA Journal
language:en
Short-container-title:AIAA Journal

Author:

Murray Alvin L.¹,Lewis Clark H.¹

Affiliation:

1. Virginia Polytechnic Institute and State University, Blacksburg, Va.

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.61044

Reference19 articles.

1. Numerical solution of the hypersonic viscous shock-layer equations

2. NUMERICAL SOLUTIONS TO THE VISCOUS SHOCK-LAYER BLUNT BODY PROBLEM WITH INERT GAS INJECTION.

3. 4Anderson, E. C. and Moss, J. N. "Numerical Solution of the Hypersonic Viscous-Shock Layer Equations for Laminar, Transitional and Turbulent Flows of a Perfect Gas over Blunt Axially Symmetric Bodies," NASA TN D-7865, Feb.1975.

4. Viscous shock layer flow in the windward plane of cones at angle of attack

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