Hypersonic Turbulent Boundary Layer with Pressure Gradients and Cross Flow
- 1 November 1972
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 10 (11) , 1393-1394
- https://doi.org/10.2514/3.50380
Abstract
No abstract availableThis publication has 2 references indexed in Scilit:
- An experimental investigation of hypersonic turbulent boundary layers in adverse pressure gradient.AIAA Journal, 1969
- Predicting turbulent compressible boundary layers in strong adverse pressure gradients.Journal of Spacecraft and Rockets, 1968