Experimental investigation of the stability of a supersonic boundary layer on a plate with blunting of the leading edge
- 1 January 1978
- journal article
- Published by Springer Nature in Fluid Dynamics
- Vol. 12 (4) , 541-545
- https://doi.org/10.1007/bf01089672
Abstract
No abstract availableKeywords
This publication has 6 references indexed in Scilit:
- Wind Tunnel Experiments Relating to Supersonic and Hypersonic Boundary-Layer TransitionAIAA Journal, 1975
- Linear Stability Theory and the Problem of Supersonic Boundary- Layer TransitionAIAA Journal, 1975
- A Program for Transition ResearchAIAA Journal, 1975
- Stability of compressible boundary layers.AIAA Journal, 1967
- Stability and transition of a supersonic laminar boundary layer on an insulated flat plateJournal of Fluid Mechanics, 1960
- An experiment on the stability of hypersonic laminar boundary layersJournal of Fluid Mechanics, 1960