Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer
- 1 September 1986
- journal article
- research article
- Published by Cambridge University Press (CUP) in Journal of Fluid Mechanics
- Vol. 170, 411-433
- https://doi.org/10.1017/s0022112086000952
Abstract
The three-dimensional interactions of weak swept oblique shock and expansion waves and a turbulent boundary layer on a flat plate are investigated. Upstream influences in a single swept interaction are found to be consistent with a model of the flow involving shock/boundary-layer interaction characteristics. The model implies that there is more rapid thickening of the boundary layer close to the shock generator and this is seen to be consistent with surface streamline patterns. It is also found that a superposition principle, which is inherent in the triple-deck model of shock/boundary-layer interactions proposed by Lighthill, can be used to predict the pressure field and surface streamlines for the case of intersecting shock interactions and for the intersection of a shock with a weak expansion.Keywords
This publication has 8 references indexed in Scilit:
- Upstream influence scaling of sharp fin-induced shock wave turbulent boundary layer interactionsPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1981
- UPSTREAM INFLUENCE AND SKIN FRICTION IN NON-SEPARATING SHOCK-TURBULENT BOUNDARY LAYER INTERACTIONSPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Interaction between a normal shock wave and a turbulent boundary layer at high transonic speeds. Part I: Pressure distributionZeitschrift für angewandte Mathematik und Physik, 1980
- Analysis of Two-Dimensional Interactions Between Shock Waves and Boundary LayersAnnual Review of Fluid Mechanics, 1980
- Analytical Theory of Transonic Normal Shock-Turbulent Boundary-Layer InteractionAIAA Journal, 1976
- A Simple Correlation for Incipient-Turbulent Boundary-Layer Separation due to a Skewed Shock WaveAIAA Journal, 1973
- The Three-Dimensional Interaction of a Shock Wave with a Turbulent Boundary LayerAeronautical Quarterly, 1966
- Sweepback Effects in Turbulent Boundary-Layer Shock-Wave InteractionJournal of the Aerospace Sciences, 1960