An effect of sudden circumferential strain on the laminar boundary layer on a rotating cylinder in an axial flow

Author:

Nakamura I.,Yamashita S.,Watanabe T.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,Computational Mechanics

Reference10 articles.

1. Nakamura, I., Yamashita, S.: Boundary layer on bodies of revolution spinning in axial flows. IUTAM Symposium on Theoretical and Applied Mechanics (Berlin, 1982), pp. 177?187. Berlin-Heidelberg-New York: Springer 1982.

2. Bissonnette, L. R., Mellor, G. L.: Experiments on the behavior of an axisymmetric turbulent boundary layer with a sudden circumferential strain. J. Fluid Mech.63, 369?413 (1974).

3. Lohmann, R. P.: The response of a developed turbulent boundary layer to local transverse surface motion. Trans. ASME, Ser. I,98-3, 354?363 (1976).

4. Arzoumanian, E., Fulachier, L., Dumas, R.: Experimental investigation of the three-dimensional turbulent boundary layer on an axially rotated cylinder. Proc. 2nd Symp. Turbulent Shear Flows4, 28 (1979).

5. Higuchi, H., Rubesin, M. W.: Behavior of a turbulent boundary layer subjected to sudden transverse strain. AIAA J.17-9, 931?941 (1979).

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