Chapter 17: Analytical Method of Solving Thin Viscous Shock Layer Equations at Low Reynolds Numbers-Reference-Cited by-同舟云学术

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Chapter 17: Analytical Method of Solving Thin Viscous Shock Layer Equations at Low Reynolds Numbers

Published:2013 Issue: Volume: Page:
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Container-title:Hypersonic Aerodynamics and Heat Transfer
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Begell House Inc.

Reference23 articles.

1. Continuum models of rarefied gas flows in problems of hypersonic aerothermodynamics;Brykina I.G.;Prikl. Mat. Mekh.,2006

2. Applicability of continuum models in the transitional regime of hypersonic flows;Brykina I.G.;Prikl. Mat. Mekh.,2009

3. Hypersonic shock-layer theory of the stagnation region at low Reynolds number;Cheng H.K.,1961

4. Cheng, H. K., The blunt body problem in hypersonic flow at low Reynolds number, IAS Paper No. 63-92, 1963.

5. Numerical solution of the hypersonic viscous shock layer equations;Davis R.T.;AIAA J.,1970

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