On the determination of the position of laminar-turbulent transition in boundary layer by optical methods-Reference-Cited by-同舟云学术

On the determination of the position of laminar-turbulent transition in boundary layer by optical methods

Published:2015-11 Issue:6 Volume:22 Page:767-770
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Bountin D. A.,Gromyko Yu. V.,Maslov A. A.,Polivanov P. A.,Sidorenko A. A.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/content/pdf/10.1134/S0869864315060128.pdf

Reference3 articles.

1. E.J. Softley, B.C. Graber, and R.E. Zempel, Experimental observation of transition of the hypersonic boundary layer, AIAA J., 1969, Vol. 7, No. 2, P. 257–263.

2. D.A. Bountin, S.V. Lukashevich, A.A. Maslov, and A.N. Shiplyuk, Effect of the cone nose bluntness and the ultrasonically absorptive coating on the transition in hypersonic boundary layer, Fluid Dynamics, 2010, Vol. 45, No. 6, P. 898–904.

3. Yu.V. Gromyko, P.A. Polivanov, A.A. Sidorenko, D.A. Bountin, and A.A. Maslov, An experimental study of the natural noise in the Transit-M hypersonic wind tunnel, Thermophysics and Aeromechanics, 2013, Vol. 20, No. 4, P. 481–493.

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