Compatibility of Transonic Flows at Thick Trailing Edge in Turbine Blade Row
نویسندگان
چکیده
منابع مشابه
Simulating Cooling Injection Effect of Trailing Edge of Gas Turbine Blade on Surface Mach Number Distribution of Blade
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Julien Christophe, Stéphane Moreau, Jérome Anthoine 1 von Karman Institute for Fluid Dynamics, 72 Chaussée de Waterloo, 1640 Rhode-St-Genèse, Belgium, [email protected] 2 Université de Sherbrooke, 2500 Boulevard de l’Université, Sherbrooke, J1K 2R1 Québec, Canada, [email protected] 3 ONERA The French Aerospace Lab, Midi-Pyrenees Center, Mauzac, France, Jerome.Anthoine@one...
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ژورنال
عنوان ژورنال: Bulletin of JSME
سال: 1983
ISSN: 0021-3764,1881-1426
DOI: 10.1299/jsme1958.26.1877