Thermodynamic performance evaluation of gas turbine cycle with transpiration cooling of blades using air vis-à-vis steam

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy

Volumn 224, Issue 8, 2010, Pages 1039-1047

  Kumar, S ^a   Singh, O ^a  

^a HARCOURT BUTLER TECHNOLOGICAL INSTITUTE   (India)

Author keywords

Cooling with air vis vis steam; Cycle performance; Gas turbine; Radiation; Transpiration cooling

Indexed keywords

COMPUTER CODES; CONVECTION COOLING; COOLING MEDIUM; COOLING TECHNIQUE; CYCLE EFFICIENCY; CYCLE PERFORMANCE; CYCLE PRESSURE RATIOS; FILM COOLING; GAS CYCLE; GAS TURBINE BLADES; GAS TURBINE CYCLES; HIGH-TEMPERATURE COMBUSTION; HIGHER TEMPERATURES; OVERALL EFFICIENCY; PERFORMANCE EVALUATION; SPECIFIC POWER; THERMODYNAMIC PERFORMANCE EVALUATION; TRANSPIRATION COOLING; TURBINE INLET TEMPERATURE;

CARBON DIOXIDE; COOLANTS; COOLING; EFFICIENCY; GAS TURBINE LOCOMOTIVES; GAS TURBINES; GASES; RADIATION; STEAM; TEMPERATURE; TRANSPIRATION;

TURBOMACHINE BLADES;

EID: 79956041042     PISSN: 09576509     EISSN: 20412967     Source Type: Journal    
DOI: 10.1243/09576509JPE964     Document Type: Conference Paper

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