Numerical studies of supersonic turbulentboundary-layer flows with tangential slot injection

DOI10.1016/0045-7825(74)90003-6zbMath0279.76030OpenAlexW2000378667MaRDI QIDQ1843211

E. W. Miner, Clark H. Lewis

Publication date: 1974

Published in: Computer Methods in Applied Mechanics and Engineering (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0045-7825(74)90003-6

Mathematics Subject Classification ID

Isotropic turbulence; homogeneous turbulence (76F05) Supersonic flows (76J20) Numerical methods for partial differential equations, boundary value problems (65N99)

Cites Work

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• A finite-difference procedure for solving the equations of the two- dimensional boundary layer
• Nonequilibrium laminar boundary-layer flow of ionized air
• Second-order boundary-layer effects in hypersonic flow past axisymmetric blunt bodies
• Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental data
• Finite difference methods of solution of the boundary-layer equations
• Calculation of compressible adiabatic turbulent boundary layers
• A survey of the mean turbulent field closure models.

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