Reynolds analogy violation for a compressible turbulent boundary layer with pressure gradient in a small-size supersonic slot channel-Reference-Cited by-同舟云学术

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Reynolds analogy violation for a compressible turbulent boundary layer with pressure gradient in a small-size supersonic slot channel

Published:2024-06 Issue: Volume:200 Page:108973
ISSN:1290-0729
Container-title:International Journal of Thermal Sciences
language:en
Short-container-title:International Journal of Thermal Sciences

Author:

Kiselev N.A.,Malastowski N.S.^ORCID,Zditovets A.G.^ORCID,Vinogradov Yu.A.

Funder

Russian Science Foundation

Publisher

Elsevier BV

Reference49 articles.

1. Boundary Layer Theory;Schlichting,1979

2. Turbulent boundary layers in adverse pressure gradients;Clauser;J. Aeronaut. Sci.,1954

3. Heat transfer and skin-friction in a turbulent boundary layer under a non-equilibrium longitudinal adverse pressure gradient;Kiselev;Int. J. Heat Fluid Flow,2021

4. Equilibrium and non-equilibrium turbulent boundary layers;Devenport;Prog. Aero. Sci.,2022

5. Heat Transfer, Mass Transfer, and Friction in Turbulent Boundary Layer;Kutateladze,1990

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1. Reynolds analogy in a packed bed for a high Prandtl number fluid;International Journal of Heat and Mass Transfer;2024-11

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