A model for adiabatic supersonic turbulent boundary layers

DOI10.1007/BF00456375zbMath0881.76045OpenAlexW2087306110MaRDI QIDQ1364180

O. Diekmann

Publication date: 28 September 1997

Published in: Theoretical and Computational Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1007/bf00456375

zbMATH Keywords

asymptotic analysisadiabatic wallalgebraic turbulence modeleffects of viscous dissipationtotal enthalpy profile

Mathematics Subject Classification ID

Shear flows and turbulence (76F10) Supersonic flows (76J20) Boundary-layer theory for compressible fluids and gas dynamics (76N20)

Cites Work

• Computation of attached three-dimensional turbulent boundary layers
• The three-dimensional turbulent boundary layer near a plane of symmetry
• The structure of a three-dimensional turbulent boundary layer
• An asymptotic two-layer model for supersonic turbulent boundary layers
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