Calculation of the unsteady burning velocity according to a known law of pressure variation during transient processes in a solid-propellant rocket engine-Reference-Cited by-同舟云学术

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Calculation of the unsteady burning velocity according to a known law of pressure variation during transient processes in a solid-propellant rocket engine

Published:2014-05 Issue:3 Volume:8 Page:345-351
ISSN:1990-7931
Container-title:Russian Journal of Physical Chemistry B
language:en
Short-container-title:Russ. J. Phys. Chem. B

Author:

Marshakov V. N.,Puchkov V. M.

Publisher

Pleiades Publishing Ltd

Subject

Physical and Theoretical Chemistry

Link

http://link.springer.com/content/pdf/10.1134/S1990793114030099.pdf

Reference17 articles.

1. T. A. Fletcher and G. W. Bunde, AIAA Paper, No. 65, 104 (1965).

2. E. A. Fletcher and D. V. Bandi, Raketn. Tekhn. Kosmon., No. 1, 227 (1966).

3. B. Dubrov et al., Vopr. Raket. Tekh., No. 1, 66 (1966).

4. K. Sherwin, Vopr. Raket. Tekh., No. 6 (1966).

5. T. A. Fletcher, AIAA J. 4, 2222 (1966).

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Experimental Study of Unsteady Burning Rate of High-Energy Materials under Depressurization;Combustion, Explosion, and Shock Waves;2023-04

2. Ignition and Combustion of Composite Solid Propellants Based on a Double Oxidizer and Boron-Based Additives;Russian Journal of Physical Chemistry B;2020-07

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