Effect of Reynolds number on boundary layer development behind an expansion fan

Author:

Gol'dfel'd M. A.,Lisenkov I. G.

Publisher

Springer Science and Business Media LLC

Subject

Fluid Flow and Transfer Processes,General Physics and Astronomy,Mechanical Engineering

Reference12 articles.

1. V. Zakkay, K. Toba, and T. J. Kuo, ?Laminar, transitional and turbulent heat transfer after a sharp convex corner,? AIAA J.,2, 1389 (1964).

2. J. Delery and B. Masure, ?Action d'une variation brusque de pression sur une couche limite turbulente et application aux prises d'air hypersoniques,? Rech. Aerosp., No. 29, 3 (1969).

3. J. P. Dussauge and J. Gaviglio, ?Bulk dilatation effect on Reynolds stresses in the rapid expansion of a turbulent boundary layer at supersonic speed,? IMST, Marseilles, 1981?113, 6 (1981).

4. E. V. Pavlyukov, ?Investigation of the turbulent boundary layer in flow over a convex corner,? Tr. TsAGI, No. 1498, 12 (1973).

5. A. A. Zheltovodov, L. Ch.-Yu. Mekler, and É. Kh. Shilein, ?Characteristics of the development of separated compression corner flows behind expansion waves,? Preprint No. 10 [in Russian], Institute of Theoretical and Applied Mechanics of the USSR Academy of Sciences, Novosibirsk (1987).

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