Theory of the hypersonic viscous shock layer at high Reynolds numbers and intensive injection of foreign gases-Reference-Cited by-同舟云学术

Theory of the hypersonic viscous shock layer at high Reynolds numbers and intensive injection of foreign gases

Published:1974-01 Issue:6 Volume:38 Page:962-972
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Gershbein E.A.

Publisher

Elsevier BV

Subject

Applied Mathematics,Mechanical Engineering,Mechanics of Materials,Modeling and Simulation

Reference28 articles.

1. The flow of viscous heat conducting multicomponent gas in the shock layer in the neighborhood of blunting in the presence of intensive injection;Gershbein;Nauch. Tr. Inst. Mekhaniki MGU,1970

2. The downstream influence of mass transfer at the nose of a slender cone;Gresci;J. Aero-Space Sci.,1962

3. Supersonic flow past blunt bodies with large surface injection;Taylor,1968

4. Intensive injection at the surface of the blunted body in a supersonic stream;Stulov,1972

5. The flow of a stream with selective radiation past smooth symmetric bodies;Olstad;Raketnaia Tekhnika i Kosmonavtika,1971

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3. Supersonic flow past axisymmetric body with strong local two-phase surface injection;Journal of Applied Mechanics and Technical Physics;1984

4. Hypersonic viscous flow past a blunt cone with massive injection at the nose;Journal of Applied Mechanics and Technical Physics;1984

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