Separation shock motion in fin, cylinder, and compression ramp - Induced turbulent interactions
- 1 June 1989
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 27 (6) , 734-742
- https://doi.org/10.2514/3.10173
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Three-dimensional shock wave turbulent boundary layer interaction for a 20 deg sharp fin at Mach 3Published by American Institute of Aeronautics and Astronautics (AIAA) ,1987
- The flowfield structure of the 3-D shock wave - Boundary layer interaction generated by a 20 deg sharp fin at Mach 3Published by American Institute of Aeronautics and Astronautics (AIAA) ,1986
- The buffeting pressure field of a high-aspect-ratio swept wingPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1985
- Unsteadiness of the shock wave structure in attached and separated compression ramp flowsExperiments in Fluids, 1985
- Simulation of blunt-fin-induced shock wave and turbulent boundary-layer interactionPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Characteristic frequencies of transonic diffuser flow oscillationsAIAA Journal, 1983
- On the structure and resolution of wall-pressure fluctuations associated with turbulent boundary-layer flowJournal of Fluid Mechanics, 1983
- Blunt fin-induced shock wave/turbulent boundary-layer interactionAIAA Journal, 1982
- Details of a Shock-Separated Turbulent Boundary Layer at a Compression CornerAIAA Journal, 1976
- Pressure fluctuations underlying attached and separated supersonic turbulent boundary layers and shock wavesPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1973