Measurements of Mach 3 Turbulence Transport Properties on a Nozzle Wall
- 1 June 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (6) , 725-729
- https://doi.org/10.2514/3.61412
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- 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 effectsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- A study of shock-wave turbulent boundary layer interaction using laser velocimeter and hot-wire anemometer techniquesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1974
- Calculation of Compressible Turbulent Boundary Layers with Heat and Mass TransferAIAA Journal, 1971
- Mixing length and kinematic eddy viscosity in a compressible boundary layer.AIAA Journal, 1968
- Turbulent Boundary Layer in Compressible FluidsJournal of the Aeronautical Sciences, 1951