On the effect of a porous insert in the supersonic section of a nozzle upon change in its thrust-Reference-Cited by-同舟云学术

On the effect of a porous insert in the supersonic section of a nozzle upon change in its thrust

Published:2005-04 Issue:4 Volume:50 Page:188-191
ISSN:1028-3358
Container-title:Doklady Physics
language:en
Short-container-title:Dokl. Phys.

Author:

Zaikovskii V. N.,Kiselev V. P.,Kiselev S. P.,Melamed B. M.,Sokolovskii M. I.,Todoshchenko A. I.,Trubacheev G. V.,Fomin V. M.

Publisher

Pleiades Publishing Ltd

Subject

General Physics and Astronomy,Mechanics of Materials,Computational Mechanics

Link

http://link.springer.com/content/pdf/10.1134/1.1922558.pdf

Reference4 articles.

1. V. V. Semenov, Tr. MAI (Élektron. Zh.), No. 1 (2000).

2. V. M. Melamed, V. N. Zaikovskii, A. I. Todoschenko, and G. V. Trubacheev, in Proceedings of the 9th International Conference on the Methods of Aerophysical Research (ITAM SB RAS, Novosibirsk, 2002), pp. 164–170.

3. G. L. Loitsyanskii, Mechanics of Liquids and Gases (Nauka, Moscow, 1987; Begell House, New York, 1995).

4. G. L. Grozdovskii, A. A. Nikol’skii, G. P. Svishchev, and G. I. Taganov, Supersonic Gas Flows in Perforated Boundaries (Mashinostroenie, Moscow, 1967) [in Russian].

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