Scaling of interactions of cylinders with supersonic turbulent boundary layers
- 1 May 1981
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 19 (5), 655-657
- https://doi.org/10.2514/3.7805
Abstract
No abstract availableKeywords
This publication has 13 references indexed in Scilit:
- Three-dimensional protuberance interference heating in high speed flowPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- An examination of blunt fin-induced shock wave turbulent boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1979
- Coherent motions in the outer region of turbulent boundary layersPhysics of Fluids, 1977
- Separation ahead of Protuberances in Supersonic Turbulent Boundary LayersAIAA Journal, 1977
- Calculation of compressible turbulent boundary layers on straight-tapered swept wingsAIAA Journal, 1976
- Mixing Length in Low Reynolds Number Compressible Turbulent Boundary LayersAIAA Journal, 1975
- The effect of mean compression or dilatation on the turbulence structure of supersonic boundary layersJournal of Fluid Mechanics, 1974
- The turbulent boundary layer with foreign gas injection—I. Measurements in zero pressure gradientInternational Journal of Heat and Mass Transfer, 1974
- Turbulent boundary-layer separation ahead of cylinders.AIAA Journal, 1968
- Some experiments on equilibrium turbulent boundary layers in favourable pressure gradientsJournal of Fluid Mechanics, 1967