Rheology of rarefied gas flow in hypersonic shock and boundary layers-Reference-Cited by-同舟云学术

Rheology of rarefied gas flow in hypersonic shock and boundary layers

Published:2007-10 Issue:5 Volume:42 Page:851-857
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Kuznetsov M. M.,Lipatov I. I.,Nikolskii V. S.

Publisher

Pleiades Publishing Ltd

Subject

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

Link

http://link.springer.com/content/pdf/10.1134/S0015462807050171.pdf

Reference19 articles.

1. V.N. Gusev, A.I. Erofeev, E.V. Klimova, et al., “Theoretical and Experimental Investigations of Hypersonic Rarefied Gas Flow around Bodies of Simple Shape,” Trans. Central Aerohydrodynamics Institute [in Russian], Is. 1855 (1977).

2. G.A. Bird, “Low Density Aerothermodynamics,” AIAA Paper No. 0994 (1985).

3. N.K. Cheng, “Hypersonic Shock-Layer Theory of the Stagnation Region at Low Reynolds Number,” in Proc. Heat Transfer and Fluid Mech. (Stanford Univ. Press, 1961) 161–175.

4. H.K. Cheng, “The Blunt Body Problem in Hypersonic Flow at Low Reynolds Number,” Paper Inst. Aerospace Sciences, No. 63–92 (1963).

5. W.B. Bush, “On the Viscous Hypersonic Blunt Body Problem,” J. Fluid Mech. 20(Pt 3), 353–367 (1964).

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