Electrogasdynamic effect on small perturbation development in the boundary layer on a thin airfoil-Reference-Cited by-同舟云学术

Electrogasdynamic effect on small perturbation development in the boundary layer on a thin airfoil

Published:1986 Issue:1 Volume:21 Page:19-26
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Kazakov A. V.,Kuryachii A. P.

Publisher

Springer Science and Business Media LLC

Subject

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

Link

http://link.springer.com/content/pdf/10.1007/BF01051095.pdf

Reference14 articles.

1. D. M. Bushnell, ?Turbulent drag reduction for external flows,? AIAA Pap., No. 227, 20 (1933).

2. A. V. Kazakov, M. N. Kogan, and V. A. Kuparev, ?Stability of the subsonic boundary layer on a flat plate with heating of the surface near the leading edge.? Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 3, 68 (1985).

3. M. R. Malik, L. M. Weinstein, and M. Y. Hussaini, ?Ion wind drag reduction,? AIAA Pap., No. 231, 10 (1983).

4. A. P. Kuryachii, ?Electrohydrodynamic postponement of boundary layer transition,? Prikl. Hat. Mekh.,49, 107 (1085).

5. A. B. Vatazhin, V. I. Grabovskii, V. A. Likhter, and V. I. Shul'gin, Electrogasdynamic Flows [in Russian], Nauka, Moscow (1983).

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