共 50 条
- [1] Heat Transfer Coefficients of Film Cooling on a Rotating Turbine Blade Model-Part I: Effect of Blowing Ratio JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2009, 131 (04): : 1 - 12
- [2] HEAT TRANSFER COEFFICIENTS OF FILM COOLING ON A ROTATING TURBINE BLADE MODEL: PART I. EFFECT OF BLOWING RATIO PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 4, PTS A AND B, 2008, : 521 - 531
- [3] EFFECT OF LOCATION AND ROTATIONAL REYNOLDS NUMBER ON FILM COOLING OF ROTATING BLADE PRESSURE SIDE PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 6A, 2022,
- [5] FILM COOLING HOLE SHAPE EFFECTS ON TURBINE BLADE HEAT TRANSFER PART II: EFFECTS OF MASS FLOW RATE AND UNSTEADINESS PROCEEDINGS OF ASME TURBO EXPO 2022: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, GT2022, VOL 6A, 2022,
- [7] Heat transfer coefficients and film cooling effectiveness on the squealer tip of a gas turbine blade JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2003, 125 (04): : 648 - 657
- [8] Heat transfer coefficients and film-cooling effectiveness on a gas turbine blade tip JOURNAL OF HEAT TRANSFER-TRANSACTIONS OF THE ASME, 2003, 125 (03): : 494 - 502
- [9] THE EFFECTS OF INLET REYNOLDS NUMBER, EXIT MACH NUMBER AND INCIDENCE ANGLE ON LEADING EDGE FILM COOLING EFFECTIVENESS OF A TURBINE BLADE IN A LINEAR TRANSONIC CASCADE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 5B, 2015,