The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number-Reference-Cited by-同舟云学术

The influence of the laminar–turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number

Published:2015-10 Issue:10 Volume:41 Page:933-937
ISSN:1063-7850
Container-title:Technical Physics Letters
language:en
Short-container-title:Tech. Phys. Lett.

Author:

Polivanov P. A.,Sidorenko A. A.,Maslov A. A.

Publisher

Pleiades Publishing Ltd

Subject

Physics and Astronomy (miscellaneous)

Link

http://link.springer.com/content/pdf/10.1134/S1063785015100120.pdf

Reference8 articles.

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2. J. E. Green, AIAA Pap. 2008-3738 (2008).

3. S. M. Aul’chenko and V. P. Zamuraev, Tech. Phys. Lett. 38, 797 (2012).

4. A. A. Zheltovodov, AIAA Pap. 2006-496 (2006).

5. D. V. Gaitonde, Progr. Aerospace Sci. 72, 80 (2015).

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