Abstract
This paper presents the results of measurements of the transient burning rate of homogeneous and model composite solid propellants during sudden depressurization of a semi-enclosed volume using two independent methods - high-speed photography and a method based on solving the inverse problem of interior ballistics. A comparative analysis of the results shows that the methods are mutually complementary.
Original language | English |
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Pages (from-to) | 570-577 |
Number of pages | 8 |
Journal | Combustion, Explosion and Shock Waves |
Volume | 46 |
Issue number | 5 |
DOIs | |
Publication status | Published - 1 Sep 2010 |
Keywords
- depressurization
- half-closed volume
- high-speed photography
- hot-spot pulsating combustion regime
- inverse problem of interior ballistics
- solid propellants
- transient burning rate
ASJC Scopus subject areas
- Chemistry(all)
- Chemical Engineering(all)
- Fuel Technology
- Energy Engineering and Power Technology
- Physics and Astronomy(all)