A Small Cross Flow Theory for Three-Dimensional, Compressible, Turbulent Boundary Layers on Adiabatic Walls
- 1 July 1973
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 11 (7) , 950-954
- https://doi.org/10.2514/3.50546
Abstract
No abstract availableThis publication has 11 references indexed in Scilit:
- A Family of Hodograph Models for the Cross Flow Velocity Component of Three-Dimensional Turbulent Boundary LayersJournal of Basic Engineering, 1972
- Entrainment Equation for Three-Dimensional, Compressible, Turbulent Boundary LayersAIAA Journal, 1972
- Crossflow profiles for compressible, turbulent boundary layersJournal of Aircraft, 1971
- Entrainment theory for compressible, turbulent boundary layers on adiabatic wallsAIAA Journal, 1971
- Discussion: “Simultaneous Lateral Skewing in a Three-Dimensional Turbulent Boundary-Layer Flow” (Klinksiek, W. F., and Pierce, F. J., 1970, ASME J. Basic Eng., 92, pp. 83–90)Journal of Basic Engineering, 1970
- Turbulent boundary-layer growth and separation on a yawed cone.AIAA Journal, 1968
- Boundary Layer Effects in the Turbulent Spiral Vortex Flow of a Compressible FluidProceedings of the Institution of Mechanical Engineers, 1968
- Approximate solutions for compressible turbulent boundary layers in three-dimensional flow.AIAA Journal, 1968
- The prediction of turbulent boundary layer development in compressible flowJournal of Fluid Mechanics, 1968
- Turbulent Heat Transfer on Blunt-Nosed Bodies in Two-Dimensional and General Three-Dimensional Hypersonic FlowJournal of the Aerospace Sciences, 1960