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机译:Cooling of Gas Turbine Blade Leading Edge Via an Array of Air Jets With Variable Diameters
South Valley Univ;
gas turbine blade leading edge; jet impingement; variable jet diameter; SST k-omega model; heat transfer uniformity; performance evaluation factor; IMPINGEMENT HEAT-TRANSFER; NUMERICAL-SIMULATION; NOZZLE SHAPE; FLOW; UNIFORMITY; ANGLE;