Shock/turbulent boundary-layer interaction with wall function boundary conditions

This publication has 11 references indexed in Scilit:

• A Wall Law for Turbulent Boundary Layers in Adverse Pressure Gradients
  AIAA Journal, 1984
• Hypersonic large-deflection similitude for quasi-wedges and quasi-cones
  The Aeronautical Journal, 1984
• Viscous shock-layer flowfield analysis by an explicit-implicit method
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1983
• A Numerical Method for Solving the Equations of Compressible Viscous Flow
  AIAA Journal, 1982
• Large incidence hypersonic similitude and oscillating nonplanar wedges
  AIAA Journal, 1980
• ON THE CALCULATION OF TURBULENT HEAT TRANSPORT DOWNSTREAM FROM AN ABRUPT PIPE EXPANSION
  Numerical Heat Transfer, 1980
• An Implicit Factored Scheme for the Compressible Navier-Stokes Equations
  AIAA Journal, 1978
• The numerical computation of turbulent flows
  Computer Methods in Applied Mechanics and Engineering, 1974
• Hypersonic Turbulent Skin-Friction and Boundary-Layer Profiles on Nonadiabatic Flat Plates
  AIAA Journal, 1972
• Stability of oscillating wedges and caret wings in hypersonic and supersonic flows.
  AIAA Journal, 1969