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Volumn 52, Issue 3-4, 2009, Pages 971-985
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Experimental study of multi-hole cooling for integrally-woven, ceramic matrix composite walls for gas turbine applications
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Author keywords
Blowing ratio; Cooling effectiveness; Integrally woven ceramic matrix composite; Reynolds number; Temperature ratio
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Indexed keywords
CERAMIC MATERIALS;
CERAMIC MATRIX COMPOSITES;
COOLING SYSTEMS;
ELECTRIC GENERATORS;
GAS TURBINES;
METALLIC MATRIX COMPOSITES;
RADIATION EFFECTS;
REYNOLDS NUMBER;
WEAVING;
BLOWING RATIO;
COOLING EFFECTIVENESS;
COOLING EFFICIENCIES;
COOLING PROCESSES;
EXPERIMENTAL STUDIES;
FLOW CONDITIONS;
GAS TURBINE APPLICATIONS;
HIGH EFFICIENCIES;
INJECTION HOLES;
INTEGRALLY-WOVEN CERAMIC MATRIX COMPOSITE;
KEY PARAMETERS;
MEAN VELOCITIES;
PARAMETER SCALING;
PRIMARY FLOWS;
SURFACE TEMPERATURES;
TEMPERATURE RATIO;
TWO TYPES;
COOLING;
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EID: 57749084482
PISSN: 00179310
EISSN: None
Source Type: Journal
DOI: 10.1016/j.ijheatmasstransfer.2008.08.008 Document Type: Article |
Times cited : (23)
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References (6)
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