Temperature of a thermally-insulated permeable wall in a compressible flow

DOI10.1134/S0015462808050141zbMath1210.76138MaRDI QIDQ532256

V. G. Lushchik, A. E. Yakubenko

Publication date: 26 April 2011

Published in: Fluid Dynamics (Search for Journal in Brave)

zbMATH Keywords

supersonic flowboundary layertemperature recovery coefficientthermally-insulated permeable wall

Mathematics Subject Classification ID

Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Related Items (1)

Experimental investigation of the temperature stratification of an air flow through a supersonic channel with a central body in the form of a porous permeable tube

Cites Work

• Transfer equation for turbulent heat flux. Calculation of heat exchange in a pipe
• Three-parameter model of shear turbulence

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