Numerical study of separated laminar boundary layers over multiple sine-wave protuberances
- 1 March 1976
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Spacecraft and Rockets
- Vol. 13 (3) , 168-173
- https://doi.org/10.2514/3.27894
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Aerodynamic heating to corrugation stiffened structures in thick turbulent boundary layersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- New Method for Supersonic Boundary-Layer SeparationsAIAA Journal, 1974
- Numerical Study of Supersonic Turbulent Boundary Layer over a Small ProtuberanceAIAA Journal, 1974
- SUPERSONIC AND HYPERSONIC TWO-DIMENSIONAL LAMINAR FLOW OVER A COMPRESSION CORNERPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973
- Initial conditions for the hypersonic-shock/boundary-layer interaction problem.AIAA Journal, 1973
- The Theory of Viscous Hypersonic FlowAnnual Review of Fluid Mechanics, 1971
- Upstream Influence in Viscous Interaction ProblemsPhysics of Fluids, 1968
- Heat transfer to wavy wall in hypersonic flow.AIAA Journal, 1967
- The laminar compressible boundary layer along a wave-shaped wallArchive of Applied Mechanics, 1963