Numerical simulation of the operation process and thrust performance of an air-breathing pulse detonation engine in supersonic flight conditions-Reference-Cited by-同舟云学术

Numerical simulation of the operation process and thrust performance of an air-breathing pulse detonation engine in supersonic flight conditions

Published:2011-08 Issue:4 Volume:5 Page:597-609
ISSN:1990-7931
Container-title:Russian Journal of Physical Chemistry B
language:en
Short-container-title:Russ. J. Phys. Chem. B

Author:

Ivanov V. S.,Frolov S. M.

Publisher

Pleiades Publishing Ltd

Subject

Physical and Theoretical Chemistry

Link

http://link.springer.com/content/pdf/10.1134/S1990793111040075.pdf

Reference20 articles.

1. Ya. B. Zel’dovich, Zh. Tekh. Fiz. 10, 1453 (1940).

2. T. Bussing and G. Pappas, in Progress in Astronautics and Aeronautics Series, Ed. by S. N. B. Murthy and E. T. Curran (AIAA Inc, Washington, DC, 1996), p. 165.

3. S. M. Frolov, “Pulse Detonation Engines: Introduction,” in Pulse Detonation Engines (Torus Press, Moscow, 2006), p. 19 [in Russian].

4. K. Kailasanath, AIAA J. 38, 1698 (2000).

5. G. D. Roy, S. M. Frolov, A. A. Borisov, and D. W. Netzer, Progr. Energy Combust. Sci. 30, 545 (2004).

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