Computation of hypersonic turbulent boundary layers with heat transfer
- 16 July 1973
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 15 references indexed in Scilit:
- Pressure-Gradient Effects on Hypersonic Turbulent Skin-Friction and Boundary-Layer ProfilesAIAA Journal, 1972
- Hypersonic Turbulent Skin-Friction and Boundary-Layer Profiles on Nonadiabatic Flat PlatesAIAA Journal, 1972
- Temperature Distributions in Supersonic Turbulent Boundary LayersAIAA Journal, 1971
- Boundary-layer Pitot and hot-wire surveys at a free-stream Mach number of about 20AIAA Journal, 1971
- Calculation of boundary-layer development using the turbulent energy equation: compressible flow on adiabatic wallsJournal of Fluid Mechanics, 1971
- Calculation of nonequilibrium hypersonic turbulent boundary layers and comparisons with experimental dataAIAA Journal, 1970
- An experimental study of the turbulent prandtl number of air with injection and suctionInternational Journal of Heat and Mass Transfer, 1970
- Temperaturverteilungen in der turbulenten grenzschicht an der ebenen platteInternational Journal of Heat and Mass Transfer, 1964
- The fluctuating pressure field in a supersonic turbulent boundary layerJournal of Fluid Mechanics, 1963
- Some properties of boundary layer flow during the transition from laminar to turbulent motionJournal of Fluid Mechanics, 1957