Influence of the unit Reynolds number on transition in a supersonic boundary layer-Reference-Cited by-同舟云学术

Influence of the unit Reynolds number on transition in a supersonic boundary layer

Published:1976 Issue:4 Volume:9 Page:625-628
ISSN:0015-4628
Container-title:Fluid Dynamics
language:en
Short-container-title:Fluid Dyn

Author:

Kharitonov A. M.,Chernykh V. V.

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/BF01031324.pdf

Reference11 articles.

1. A. Henderson, ?Hypersonic viscous flows,? in: Current Problems of Gas dynamics,? [Russian translation], Mir, Moscow (1971).

2. V. Ya. Borova, ?The influence of the unit Reynolds number on measurements of the aerodynamic and thermal characteristics of bodies in wind tunnels,? Trudy Tsentral'nogo Aérogidrodinamicheskogo Instituta, Issue 1374, No. 5 (1972).

3. V. V. Struminskii, A. M. Kharitonov, and V. V. Chernykh, ?Experimental study of the transition of a laminar boundary layer into a turbulent one at supersonic velocities,? Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 2 (1972).

4. S. R. Pate and C. J. Schueler, ?Radiated aerodynamic noise effects on boundary-layer transition in supersonic and hypersonic wind tunnels,? AIAA J.7, No. 3 (1969).

5. V. I. Kornilov, V. Ya. Levchenko, and A. M. Kharitonov, ?Study of boundary-layer transition on wing profile at supersonic velocities,? Izv. Sibirsk. Otd. Akad. Nauk SSSR, Ser. Tekh. Nauk,1, No. 3 (1971).

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