Numerical investigation of the influence of crystallization of ultrafine particles of aluminum oxide on energy characteristics of solid-propellant rocket engine-Reference-Cited by-同舟云学术

Numerical investigation of the influence of crystallization of ultrafine particles of aluminum oxide on energy characteristics of solid-propellant rocket engine

Published:2014-08 Issue:4 Volume:21 Page:509-513
ISSN:0869-8643
Container-title:Thermophysics and Aeromechanics
language:en
Short-container-title:Thermophys. Aeromech.

Author:

Dyachenko N. N.,Dyachenko L. I.

Publisher

Pleiades Publishing Ltd

Subject

Nuclear and High Energy Physics,Radiation

Link

http://link.springer.com/content/pdf/10.1134/S0869864314040118.pdf

Reference13 articles.

1. M.Yu. Reizer, V.N. Strunin, and T.B. Manelis, Possibility of crystallization of condensed combustion products in nozzles, Combustion, Explosion and Shock Waves, 1973, No. 3, P. 314–319.

2. S.V. Henderson, Effect of crystallization kinetics on rocket performance, AIAA J., 1977, Vol. 15, No. 4, P. 600–602.

3. L.E. Sternin, Fundamentals of Gas Dynamics of Two-Phase Flows in Nozzles, Mashinostroenie, Moscow, 1974.

4. V.A. Volkov, V.A. Muslaev, and U.G. Pirumov, Mathematical models of particles crystallization in two-phase flows, Fluid Dynamics, 1989, No. 6. P. 887–894.

5. V.E. Alemasov, A.F. Dregalin, and A.P. Tishin, Theory of Rocket Engines, Mashinostroenie, Moscow, 1989.

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