Comparison of methods of flight simulation using a combustion heated facility-Reference-Cited by-同舟云学术

Comparison of methods of flight simulation using a combustion heated facility

Published:2014-03 Issue:2 Volume:50 Page:144-149
ISSN:0010-5082
Container-title:Combustion, Explosion, and Shock Waves
language:en
Short-container-title:Combust Explos Shock Waves

Author:

Aleksandrov V. Yu.,Moseev D. S.

Publisher

Pleiades Publishing Ltd

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Link

http://link.springer.com/content/pdf/10.1134/S001050821402004X.pdf

Reference13 articles.

1. T. Kármán, “Basic Equations of Aero Thermochemcistry,” in Problems of Rocket Propellant Combustion (Izd. Inostr. Lit., Moscow, 1969) [Russian translation].

2. G. K. D’yakonov, Problems of Similarity Theory in Physicochemical Processes (Izd. Akad. Nauk SSSR, Moscow, 1956) [in Russian].

3. B. V. Alekseev and A. M. Grishin, Physical Gas Dynamics of Reactive Media (Vysshaya Shkola, Moscow, 1985) [in Russian].

4. V. Yu. Aleksandrov and A. N. Prokhorov, et al., “Ground Tests of Hypersonic Engines and Their Components,” in TsIAM. Scientific Contribution to the Design of Aircraft Engines (Mashinostroenie, Moscow, 2000) [in Russian].

5. Thermodynamic Properties of Individual Substances: A Manual, Ed. by V. P. Glushko (Nauka, Moscow, 1978) [in Russian].

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