Active Control of Swept Shock Wave / Boundary Layer Interactions

Author:

Babinsky H.

Publisher

Springer Berlin Heidelberg

Reference7 articles.

1. E. Stanewsky, J. Délery, J. Fulker, and W. Geissler (Ed.), “EUROSHOCK-Drag Reduction by Passive Shock Control”, Results of the Project EUROSHOCK, AER 2-CT92–0049, Notes on Numerical Fluid Mechanics, Vol. 56, Vieweg und Sohn, Braunschweig/Wiesbaden, 1997.

2. Dawes, W.N., “A Numerical Analysis of the Three-Dimensional Viscous Flow in a Transonic Compressor Rotor and Comparison with Experiment”, Trans. ASME, J. Turbomachinery, Vol. 109, 1997, pp. 83–90.

3. Leung, A.W.C. and Squire, L.C., “Reynolds Number Effects in Swept-ShockWave/Turbulent-Boundary-Layer Interaction”, AIAA Journal, Vol. 33, 1995, pp. 798–804.

4. Holmes, S.C. and Squire, L.C, “Numerical Studies of the Supersonic Flow over a Compression Corner”, Aeronautical Journal, Vol. 96, 1992, pp. 87–95.

5. Chokani, N. and Squire, L. C., “Transonic Shockwave/Turbulent Boundary Layer Interactions on a Porous Surface”, Aeronautical Journal, May 1993, pp. 163–170.

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