Asymptotic Investigation of the Thin Viscous Shock Layer Equations in the Neighborhood of the Stagnation Point for Low Reynolds Numbers-Reference-Cited by-同舟云学术

Asymptotic Investigation of the Thin Viscous Shock Layer Equations in the Neighborhood of the Stagnation Point for Low Reynolds Numbers

Published:2005-11 Issue:6 Volume:40 Page:965-972
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Brykina I. G.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Link

http://link.springer.com/content/pdf/10.1007/s10697-006-0011-5.pdf

Reference7 articles.

1. I. G. Brykina, “Asymptotic solution of the thin viscous shock layer equations at low Reynolds numbers for a cold surface,” Fluid Dynamics, 39, No.5, pp. 815–826 (2004).

2. G. A. Tirskiy, “Continuum models in problems of hypersonic rarefied gas flow around blunt bodies,” Prikl. Mat. Mekh., 61, No.6, pp. 903–930 (1997).

3. G. A. Tirskiy, “Continuum models for the problem of hypersonic flow of rarefied gas over blunt body,” Systems Analysis Modelling Simulation, 34, No.2, pp. 205–240 (1999).

4. H. K. Cheng, “Hypersonic shock-layer theory of the stagnation region at low Reynolds number,” Proc. 1961 Heat Transfer and Fluid Mech. Inst., Stanford Univ. Press, Stanford, Calif., 161–175 (1961).

5. J. N. Moss and G. A. Bird, “Direct simulation of transitional flow for hypersonic reentry conditions,” AIAA Paper, No. 84-0223 (1984).

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