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Volumn , Issue , 2004, Pages
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Performance of a supersonic model combustor using vaporized kerosene injection
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Author keywords
[No Author keywords available]
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Indexed keywords
COMBUSTION EFFICIENCIES;
COMBUSTION ENHANCEMENT;
COMBUSTOR PERFORMANCE;
COMPUTED FLOWS;
CONTROLLING MECHANISM;
CROSS FLOWS;
EFFERVESCENT ATOMIZATION;
EXPERIMENTAL DATA;
HEATING SYSTEM;
INJECTION PRESSURES;
KEROSENE INJECTION;
MODEL COMBUSTOR;
PARAMETRIC STUDY;
PENETRATION DEPTH;
PREHEAT TEMPERATURE;
QUIESCENT ENVIRONMENTS;
SONIC NOZZLE;
SUPERSONIC COMBUSTION;
SURROGATE FUELS;
THERMO-PHYSICAL PROPERTY;
THERMODYNAMIC CONDITIONS;
THREE-COMPONENT;
TWO STAGE;
VAPOR PHASE;
COMBUSTION;
COMBUSTORS;
FLOW RATE;
FUELS;
HYDROGEN;
JETS;
LIQUIDS;
PREHEATING;
PROPULSION;
RAMJET ENGINES;
SMOKE;
THERMOCHEMISTRY;
THERMODYNAMIC PROPERTIES;
VAPORS;
KEROSENE;
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EID: 77957851554
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: None Document Type: Conference Paper |
Times cited : (8)
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References (8)
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