On stability of the supersonic boundary layer with a foreign gas injection-Reference-Cited by-同舟云学术

On stability of the supersonic boundary layer with a foreign gas injection

Published:2016 Issue: Volume: Page:
ISSN:0094-243X
Container-title:AIP Conference Proceedings
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Gaponov Sergey A.,Smorodsky Boris V.

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Reference16 articles.

1. Effect of Diffusion Fields on the Laminar Boundary Layer

2. E.R.G. Eckert and P.J. Schneider, J.Aero.Sci., 23, 384–387 (1956).

3. C.R. Faulders, J.Aero.Space Sci., 28, 166–167 (1961).

4. I. Korobkin, “The effects of the molecular properties of an injected gas on compressible laminar boundary layer skin friction and heat transfer”, U.S. Naval Ordnance Laboratory Report 7410 (1961).

5. A.H. Craven, “The compressible laminar boundary layer with foreign gas injection”, College of Aeronautics, Cranfield, Report No.155 (1962).

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