An experimental investigation of the Reynolds number effect on a normal shock wave-turbulent boundary layer interaction on a curved wall

Author:

Doerffer P.,Zierep J.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference24 articles.

1. Ackeret, J., Feldmann, F., Rott, H.: Untersuchungen an Verdichtungsstößen und Grenzschichten in schnell bewegten Gasen. Bericht No. 10 des Instituts für Aerodynamik, ETH Zürich (1946).

2. Seddon, J.: The flow produced by interactions of a turbulent boundary layer with a normal shock wave of strength sufficient to cause separation. ARC R and M 3502 (1967).

3. Kooi, J. W.: Influence of free-stream Mach number on transonic shock-wave boundary-layer interaction. NRL MP 78012U.

4. Padova, C., Falk, T. J., Transonic shock wave-boundary layer interactions. AFOSRTR-80-0694 (1980).

5. Padova, C., Falk, T. J., Wittliff, C. E.: Experimental investigation of similitude parameters governing transonic shock-boundary layer interactions. AIAA Paper80-0158 (1980).

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