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Transient modes of double-base propellant combustion in a semiclosed volume

Experimental data on the transient combustion of double-base propellants in a semiclosed space are presented. The transient process is initiated by a sharp change in the cross sectional area of the nozzle. The pressure in the combustion chamber at various ratios between the initial and final cross s...

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Published in:Russian journal of physical chemistry. B 2011-02, Vol.5 (1), p.45-56
Main Authors: Marshakov, V. N., Novozhilov, B. V.
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Language:English
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Novozhilov, B. V.
description Experimental data on the transient combustion of double-base propellants in a semiclosed space are presented. The transient process is initiated by a sharp change in the cross sectional area of the nozzle. The pressure in the combustion chamber at various ratios between the initial and final cross sectional areas of the nozzle is measured. An attempt to explain the experimental data obtained within the framework of the phenomenological theory of non-steady-state combustion of energetic condensed systems is undertaken. A comparison of experimental and theoretical results demonstrates their satisfactory agreement.
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identifier ISSN: 1990-7931
ispartof Russian journal of physical chemistry. B, 2011-02, Vol.5 (1), p.45-56
issn 1990-7931
1990-7923
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subjects Chemistry
Chemistry and Materials Science
Combustion
Explosion
Physical Chemistry
Shock Waves
title Transient modes of double-base propellant combustion in a semiclosed volume
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