An Experimental Study of the Turbulent Boundary Layer Behind the Initial Shock Wave in a Shock Tube-Reference-Cited by-同舟云学术

An Experimental Study of the Turbulent Boundary Layer Behind the Initial Shock Wave in a Shock Tube

Published:1958-10 Issue:10 Volume:25 Page:644-652
ISSN:1936-9999
Container-title:Journal of the Aerospace Sciences
language:en
Short-container-title:Journal of the Aerospace Sciences

Author:

MARTIN WALTER A.¹

Affiliation:

1. University of Toronto,

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Link

http://arc.aiaa.org/doi/pdf/10.2514/8.7818

Reference24 articles.

1. Trimpi, R. L., and Cohen, N. B., A Theory for Predicting the Flow of Real Gases in Shock Tubes with Experimental Verification, N A C A T N 3375,1955.

2. Bershader, D., and Allport, J., On the Laminary Boundary Layer Induced by a Traveling Shock Wave, Princeton University, Dept. of Physics, Tech. Report 11-22, 1956.

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