Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inlet-Reference-Cited by-同舟云学术

Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inlet

Published:2018-01 Issue:1 Volume:25 Page:31-46
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Mazhul I. I.,Gounko Yu. P.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/article/10.1134/S0869864318010031/fulltext.html

Reference17 articles.

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2. K. Matsuo, Y. Miyazato, and H.-D. Kim, Shock train and pseudo-shock phenomena in internal gas flows, Pro-gress in Aerospace Sci., 1999, No. 35, P. 33–100.

3. V.I. Penzin, Experimental Investigation of Separated Flows in Ducts, TsAGI, Moscow, 2009.

4. W. Huang, Zh.-G. Wang. M. Pourkashanian, L. Ma, D.B. Ingham, Sh.-B. Luo, J. Lei, and J. Liu, Numerical investigation of the shock wave transition in a three-dimensional scramjet isolator, Acta Astronautica, 2011, Vol. 68, Nos. 11-12, P. 1669–1675.

5. C.P. Wang, X.-A. Tian, K.-M. Cheng, and Y.-Z. Wu, Numerical analysis of pseudo-shock flow diffusion phe-nomenon in variable cross section ducts, J. Aerospace Engng, 2008, Vol. 222, No. 8, P. 1109–1121.

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