A nonasymptotic triple deck model for supersonic boundary-layer interaction
- 1 June 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 14 (6) , 767-775
- https://doi.org/10.2514/3.7150
Abstract
No abstract availableKeywords
This publication has 16 references indexed in Scilit:
- New Method for Supersonic Boundary-Layer SeparationsAIAA Journal, 1974
- Momentum Integral Method for Viscous-Inviscid Interactions with Arbitrary Wall CoolingAIAA Journal, 1974
- Base pressure in laminar supersonic flowJournal of Fluid Mechanics, 1973
- On self‐induced separation IIMathematika, 1973
- Theory of laminar viscous-inviscid interactions in supersonic flowAIAA Journal, 1969
- On the two-dimensional viscous counterpart of the one-dimensional sonic throatJournal of Fluid Mechanics, 1969
- Upstream Influence in Viscous Interaction ProblemsPhysics of Fluids, 1968
- The interaction of a shock wave with a laminar boundary layer†International Journal of Non-Linear Mechanics, 1968
- Experimental investigation of supersonic laminar, two-dimensional boundary-layer separation in a compression corner with and without cooling.AIAA Journal, 1968
- On boundary layers and upstream influence II. Supersonic flows without separationProceedings of the Royal Society of London. Series A. Mathematical and Physical Sciences, 1953