Reynolds number effect on separation structures at normal shock wave/turbulent boundary-layer interaction
- 1 September 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (9) , 1206-1212
- https://doi.org/10.2514/3.10247
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- An experimental investigation of the Reynolds number effect on a normal shock wave-turbulent boundary layer interaction on a curved wallActa Mechanica, 1988
- Topological classification of flow separation on three-dimensional bodiesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- Structural Stability of Three-Dimensional Vortex FlowsPublished by Springer Nature ,1985
- Topological structures of three-dimensional vortex flow separationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1983
- Die Ablösungsbedingung von GrenzschichtenPublished by Springer Nature ,1958