A comparison of the models of a thin and a complete viscous shock layer in the problem of the supersonic flow of a viscous gas past blunt cones-Reference-Cited by-同舟云学术

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A comparison of the models of a thin and a complete viscous shock layer in the problem of the supersonic flow of a viscous gas past blunt cones

Published:1989-01 Issue:6 Volume:53 Page:762-767
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Tirskii G.A.,Utyuzhnikov S.V.

Publisher

Elsevier BV

Subject

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

Reference16 articles.

1. Supersonic flows past bodies at small and moderate Reynolds numbers;Gershbein;Itogi Nauki i Tekhniki. Mekhanika zhidkosti i gaza. VINITI,1985

2. Three-dimensional problems of super- and hypersonic flows of a viscous gas past bodies;Peigin;Itogi Nauki i Tekhniki. Mekhanika zhidkosti i gaza. VINITI,1988

3. On the viscous hypersonic blunt body problem;Bush;J. Fluid Mech.,1964

4. On the theory of hyersonic viscous, chemically reactive gas flow with injection, past plane and axisymmetric blunt bodies;Tirskii;Nauch. Tr. In-ta Mekhan., MGU,1975

5. Non-Navier Stokes viscous flow computations;Davis;Comput. and Fluids,1980

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. On a modified shock front problem for the compressible Navier-Stokes equations;Quarterly of Applied Mathematics;2004

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