Effects of Pressure Gradient on Stability and Skin Friction in Laminar Boundary Layers in Compressible Fluids
- 1 May 1951
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aeronautical Sciences
- Vol. 18 (5) , 311-318
- https://doi.org/10.2514/8.1947
Abstract
No abstract availableKeywords
This publication has 3 references indexed in Scilit:
- Stability of Boundary Layers and of Flow in Entrance Section of a ChannelJournal of the Aeronautical Sciences, 1948
- Concerning the effect of compressibility on lam inar boundary layers and their separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1948
- Laminar boundary-layer oscillations and transition on a flat plateJournal of Research of the National Bureau of Standards, 1947