Crossflow profiles for compressible, turbulent boundary layers
- 1 March 1971
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 8 (3) , 188-189
- https://doi.org/10.2514/3.44252
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Use of Coles' universal wake function for compressible turbulent boundary layersJournal of Aircraft, 1970
- 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