Detection of turbulent boundary-layer separation using fluctuating wall pressure signals
- 1 June 1990
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 28 (6), 1052-1056
- https://doi.org/10.2514/3.25164
Abstract
No abstract availableThis publication has 10 references indexed in Scilit:
- Separation shock dynamics in Mach 5 turbulent interactions induced by cylindersAIAA Journal, 1989
- Separation shock motion in fin, cylinder, and compression ramp - Induced turbulent interactionsAIAA Journal, 1989
- Interpretation of separation lines from surface tracers in a shock-induced turbulent flowAIAA Journal, 1987
- Structure of the wall pressure fluctuations in a shock-induced separated turbulent flowPublished 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
- Unsteadiness of the Separation Shock Wave Structure in a Supersonic Compression Ramp FlowfieldAIAA Journal, 1983
- A New Probe for Measurement of Velocity and Wall Shear Stress in Unsteady, Reversing FlowJournal of Fluids Engineering, 1981
- Scaling of interactions of cylinders with supersonic turbulent boundary layersAIAA Journal, 1981
- A Wall-Flow-Direction Probe for Use in Separating and Reattaching FlowsJournal of Fluids Engineering, 1979
- Incipient separation of a supersonic turbulent boundary layer at moderate to high Reynolds numbersPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1975