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Volumn 1, Issue , 2000, Pages
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The control of shroud leakage flows to reduce aerodynamic losses in a low aspect ratio, shrouded axial flow Turbine
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Author keywords
[No Author keywords available]
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Indexed keywords
AIRCRAFT ENGINES;
ASPECT RATIO;
AXIAL FLOW TURBOMACHINERY;
FIGHTER AIRCRAFT;
LEAKAGE (FLUID);
TURBINE COMPONENTS;
TURBINES;
TURBOMACHINE BLADES;
AXIAL FLOW TURBINES;
BRAKE EFFICIENCIES;
DEVELOPMENT AND TESTING;
EXPERIMENTAL INVESTIGATIONS;
LEAKAGE FRACTION;
PROVIDE GUIDANCES;
SHROUD LEAKAGE FLOW;
SHROUDED TURBINE;
AERODYNAMICS;
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EID: 84955327526
PISSN: None
EISSN: None
Source Type: Conference Proceeding
DOI: 10.1115/2000-GT-0475 Document Type: Conference Paper |
Times cited : (34)
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References (7)
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