Characteristics of the Compressible Shear Layer over a Cavity
- 1 May 2001
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 39 (5) , 846-856
- https://doi.org/10.2514/2.1388
Abstract
No abstract availableThis publication has 25 references indexed in Scilit:
- LETTER TO THE EDITOR: CAVITY PRESSURE OSCILLATIONS: THE GENERATING MECHANISM VISUALIZEDJournal of Sound and Vibration, 1996
- Compressible cavity flow oscillation due to shear layer instabilities and pressure feedbackAIAA Journal, 1995
- Experiments in nonreacting compressible shear layersAIAA Journal, 1993
- Interference flows past cylinder-fin-sting-cavity assembliesJournal of Aircraft, 1992
- Structure of the Compressible Turbulent Shear LayerAIAA Journal, 1991
- The compressible turbulent shear layer: an experimental studyJournal of Fluid Mechanics, 1988
- Numerical simulation of supersonic flow over a three-dimensional cavityAIAA Journal, 1988
- On density effects and large structure in turbulent mixing layersJournal of Fluid Mechanics, 1974
- An evaluation of theories for predicting turbulent skin friction andheat transfer on flat plates at supersonic and hypersonic Mach numbersAIAA Journal, 1971
- Drag of rectangular cavities in supersonic and transonic flow including the effects of cavity resonanceAIAA Journal, 1970