Predicting turbulent compressible boundary layers in strong adverse pressure gradients.
- 1 August 1968
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 5 (8) , 959-963
- https://doi.org/10.2514/3.29395
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Compressible turbulent boundary layer with pressure gradient and heat transfer.AIAA Journal, 1966
- The Effect of Adverse Pressure Gradients on the Characteristics of Turbulent Boundary Layers in Supersonic StreamsJournal of the Aerospace Sciences, 1962
- A METHOD OF CALCULATING TURBULENT-BOUNDARY-LAYER GROWTH AT HYPERSONIC MACH NUMBERSPublished by Defense Technical Information Center (DTIC) ,1959