The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow-Reference-Cited by-同舟云学术

The effect of surface curvature on the boundary conditions in the viscous shock layer model for hypersonic rarefied gas flow

Published:2012-01 Issue:6 Volume:76 Page:677-687
ISSN:0021-8928
Container-title:Journal of Applied Mathematics and Mechanics
language:en
Short-container-title:Journal of Applied Mathematics and Mechanics

Author:

Brykina I.G.,Rogov B.V.,Tirskiy G.A.,Utyuzhikov S.V.

Publisher

Elsevier BV

Subject

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

Reference16 articles.

1. Continuum models of rarefied gas flows in problems of hypersonic aerothermodynamics;Brykina;J Appl Math Mech,2006

2. Asymptotic investigation of the equations of a thin viscous shock layer at low Reynolds numbers in the neighbourhood of the stagnation point;Brykina;Izv Ross Akad Nauk MZhG,2005

3. The applicability of continuum models in the transitional regime of hypersonic flow over blunt bodies;Brykina;J Appl Math Mech,2009

4. Hypersonic shock-layer theory of the stagnation region at Reynolds number;Cheng,1961

5. The blunt body problem in hypersonic viscous flow at low Reynolds number;Cheng;IAS Paper,1963

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