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Volumn 27, Issue 2, 1998, Pages 2335-2341
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Transient combustion response of homogeneous solid propellant to acoustic oscillations in a rocket motor
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Author keywords
[No Author keywords available]
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Indexed keywords
ACOUSTIC INTENSITY MEASUREMENT;
GASES;
LAMINAR FLOW;
OSCILLATING FLOW;
ROCKET ENGINES;
SOLID PROPELLANTS;
TRANSIENT ANALYSIS;
ACOUSTIC WAVE EFFECTS;
COMPUTATIONAL FLUID DYNAMICS;
FLAME RESEARCH;
GAS DYNAMICS;
HEAT RADIATION;
OSCILLATIONS;
REACTION KINETICS;
ACOUSTIC OSCILLATION;
COMBUSTION RESPONSE;
CONSERVATION EQUATIONS;
HEAT RELEASE DISTRIBUTION;
PROPELLANT BURNING RATE;
PROPELLANT SURFACES;
TEMPERATURE VARIATION;
TRANSPORT PHENOMENA;
COMBUSTION;
FLAME DYNAMICS;
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EID: 0032262339
PISSN: 00820784
EISSN: None
Source Type: Journal
DOI: 10.1016/S0082-0784(98)80084-2 Document Type: Conference Paper |
Times cited : (10)
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References (18)
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