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Volumn , Issue , 2008, Pages 237-244
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Thermodynamic evaluation of different gas turbine blade cooling techniques
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Author keywords
[No Author keywords available]
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Indexed keywords
BLADE COOLING;
COMPARATIVE EVALUATIONS;
COMPRESSOR PRESSURE RATIO;
COMPUTER CODES;
COOLANT TEMPERATURE;
COOLING EFFECTIVENESS;
COOLING MEDIUM;
COOLING TECHNIQUE;
FILM COOLING;
GAS PROPERTIES;
GAS TURBINE BLADES;
GAS TURBINE CYCLES;
GAS TURBINE MODELS;
GAS TURBINE TECHNOLOGIES;
INDEPENDENT VARIABLES;
NEW MATERIAL;
OVERALL EFFICIENCY;
SPECIFIC POWER;
THERMODYNAMIC EVALUATION;
TURBINE BLADE;
TURBINE BLADE COOLING;
COLD STORAGE;
COMPRESSED AIR;
COOLING;
GAS TURBINES;
GASES;
SEMICONDUCTOR QUANTUM DOTS;
TURBOMACHINE BLADES;
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EID: 70449652407
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1109/THETA.2008.5167172 Document Type: Conference Paper |
Times cited : (18)
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References (6)
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