LII. Experiments on two-dimensional supersonic flow in corners and over concave surfaces-Reference-Cited by-同舟云学术

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LII. Experiments on two-dimensional supersonic flow in corners and over concave surfaces

Published:1952-05 Issue:340 Volume:43 Page:568-580
ISSN:1941-5982
Container-title:The London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science
language:en
Short-container-title:The London, Edinburgh, and Dublin Philosophical Magazine and Journal of Science

Author:

Johannesen N.H.

Publisher

Informa UK Limited

Link

http://www.tandfonline.com/doi/pdf/10.1080/14786440508520212

Reference8 articles.

1. XXVIII. The conditions at a sharp leading edge in supersonic flow

2. III. The interaction between an oblique shock-wave and a turbulent boundary-layer

3. Courant , R. and Friedrichs , K.O. 1948.Supersonic Flow and Shock Waves, Interscience464–464.

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3. Shock Waves in Gases;Handbook of Shock Waves;2001

4. Supersonic Boundary-Layer Examples;Analytical Fluid Dynamics, Second Edition;2000-12-21

5. Upstream influence in boundary layers 45 years ago;Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences;2000-12-15

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