Unsteadiness of the shock wave structure in attached and separated compression ramp flowfields
- 12 July 1983
- conference paper
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 3 references indexed in Scilit:
- Wall pressure fluctuations in a supersonic separated compression ramp flowfieldPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1982
- Incipient separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975
- Fluctuating Wall Pressure under a Separated Supersonic FlowThe Journal of the Acoustical Society of America, 1964