Hypersonic Aerodynamics and Heat Transfer 2013
DOI: 10.1615/978-1-56700-309-3.278
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Chapter 15: Modeling of Turbulent Compressible Near-Wall Flows

Abstract: Semiempirical turbulence models for numerical calculation of near-wall flows of a compressible gas are presented. Various issues of modification of both algebraic and differential models, which were originally developed for low-velocity flows, to studying supersonic and hypersonic near-wall flows with intense heat exchange with the surface and the applicability limits of these models determined by the free-stream parameters and the temperature factor of the surface are considered.Semiempirical turbulence model… Show more

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