Evaluation of the turbulent transport terms for a two-dimensional nozzle wall boundary-layer flow at Mach 5 and with pressure gradient, heat transfer and upstream effects

This publication has 12 references indexed in Scilit:

• Reynolds Stress Measurements in a Hypersonic Boundary Layer
  AIAA Journal, 1973
• Measurement of turbulence transport properties in a supersonic boundary-layer flow using laser velocimeter and hot-wire anemometer techniques
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973
• Calculations of turbulent shear stress in supersonic turbulent boundary layer zero and adverse pressure gradient flow
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1973
• Effect of pressure gradient on mixing length for equilibrium turbulent boundary layers
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1972
• Temperature Distributions in Supersonic Turbulent Boundary Layers
  AIAA Journal, 1971
• Evaluation of several eddy viscosity models through comparison with measurements in hypersonic flows
  Published by American Institute of Aeronautics and Astronautics (AIAA) ,1969
• VELOCITY PROFILE, SKIN-FRICTION BALANCE AND HEAT-TRANSFER MEASUREMENTS OF THE TURBULENT BOUNDARY LAYER AT MACH 5 AND ZERO-PRESSURE GRADIENT
  Published by Defense Technical Information Center (DTIC) ,1969
• CODAG PROPULSION MACHINERY FOR ROYAL DANISH NAVY FRIGATES
  Naval Engineers Journal, 1968
• NUMERICAL SOLUTION OF THE TURBULENT-BOUNDARY-LAYER EQUATIONS
  Published by Defense Technical Information Center (DTIC) ,1967
• Fluctuation Measurements in a Supersonic Turbulent Boundary Layer
  Physics of Fluids, 1959