Glancing interactions between single and intersecting oblique shock waves and a turbulent boundary layer

Author:

Mee D. J.,Stalker R. J.,Stollery J. L.

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.

Publisher

Cambridge University Press (CUP)

Subject

Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics

Reference17 articles.

1. Lighthill M. J. 1963 Introduction to Laminar Boundary Layer Theory. In Laminar Boundary Layers .pp.46–109 (ed. L. Rosenhead ).Oxford University Press.

2. Dolling, D. S. & Bogdonoff S. M. 1981 Upstream influence scaling of sharp fin-induced shock wave turbulent boundary layer interactions.AIAA Paper 81–0336.

3. Inger G. R. 1980 Upstream influence and skin friction in non-separating shock-turbulent boundary layer interactions.AIAA Paper 80–1411.

4. Stalker R. J. 1958 Shock boundary layer interactions in three dimensions. PhD thesis, Dept. Aero. Eng. University of Sydney.

5. Lighthill M. J. 1953 On boundary layers and upstream influence II. Supersonic flows without separation Proc. R. Soc. Lond. A217,478–507.

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