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Volumn 22, Issue 2, 2001, Pages 143-155
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Prediction of effect of swirl on flow and heat transfer in a rotating cavity
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Author keywords
[No Author keywords available]
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Indexed keywords
BOUNDARY LAYERS;
COOLING SYSTEMS;
GAS TURBINES;
HEAT TRANSFER;
NOZZLES;
NUSSELT NUMBER;
PRESSURE DISTRIBUTION;
RADIAL FLOW;
ROTATING DISKS;
THERMODYNAMICS;
TURBULENCE;
ROTATING TURBINE BLADES;
TURBOMACHINE BLADES;
GAS TURBINE;
HEAT TRANSFER;
ROTATING CAVITY;
SWIRLING FLOW;
THERMODYNAMICS;
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EID: 0035310866
PISSN: 0142727X
EISSN: None
Source Type: Journal
DOI: 10.1016/S0142-727X(00)00076-X Document Type: Article |
Times cited : (84)
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References (17)
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