Laminar Boundary Layer behind Strong Shock Moving with Nonuniform Velocity-Reference-Cited by-同舟云学术

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Laminar Boundary Layer behind Strong Shock Moving with Nonuniform Velocity

Published:1962 Issue:1 Volume:5 Page:91
ISSN:0031-9171
Container-title:Physics of Fluids
language:en
Short-container-title:Phys. Fluids

Author:

Mirels Harold,Hamman Jesse

Publisher

AIP Publishing

Subject

General Engineering

Reference12 articles.

1. R. N. Hollyer, Jr., “A study of attenuation in the shock tube,” Engineering Research Institute, University of Michigan, 1953.

2. H. Mirels, NACA TN 3401 (1955).

3. H. Mirels, NACA TN 3712 (1956).

4. H. Mirels, “The wall boundary layer behind a moving shock wave,” inBoundary Layer Research, Proceedings International Union of Theoretical and Applied Mechanics, edited by H. Görtler (Springer-Verlag, Berlin, 1958), pp. 283–293.

5. H. Mirels, NASA TN D-291 (1961).

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