Stability of Compressible Boundary Layers Induced by a Moving Wave
- 1 March 1962
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of the Aerospace Sciences
- Vol. 29 (3), 289-296
- https://doi.org/10.2514/8.9410
Abstract
No abstract availableKeywords
This publication has 4 references indexed in Scilit:
- The wall boundary layer behind a moving shock wavePublished by Springer Nature ,1958
- Experiments on Boundary-Layer Transition at Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- On Transition Experiments at Moderate Supersonic SpeedsJournal of the Aeronautical Sciences, 1957
- On the Stability of the Laminar Boundary Layer in a Compressible FluidJournal of the Aeronautical Sciences, 1955