Supersonic boundary layer on a plate. Comparison of calculation and experiment-Reference-Cited by-同舟云学术

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Supersonic boundary layer on a plate. Comparison of calculation and experiment

Published:1998-11 Issue:6 Volume:33 Page:864-875
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Lushchik V. G.,Yakubenko A. E.

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/BF02698655.pdf

Reference19 articles.

1. A. S. Ginevskii, V. A. Ioselevich, A. V. Kolesnikov, et al., “Methods for calculating the turbulent boundary layer,” in:Itogi Nauki i Tekh. Mekh. Zhidk. Gaza [in Russian],11, VINITI, Moscow (1978), pp. 155–304.

2. V. M. Ievlev,Turbulent Motion of a High-Temperature Continuum [in Russian], Nauka, Moscow (1990).

3. V. S. Avduevskii, “Method for calculating the turbulent 3-D boundary layer in a compressible gas,”Izv. Akad. Nauk SSSR, OTN, Mekh. Mashinostr., No. 4, 3 (1962).

4. S. S. Kutateladze and A. I. Leont’ev,Heat-Mass Transfer and Friction in a Turbulent Boundary Layer [in Russian], Energiya, Moscow (1972).

5. V. G. Lushchik, A. A. Pavel’ev, and A. E. Yakubenko, “Three-parameter model of shear turbulence,”Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 13 (1978).

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1. Numerical investigation of the effect of the Prandtl number on the temperature recovery and the Reynolds analogy factors in the boundary layer on a plate;High Temperature;2016-05

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