共 50 条
- [41] Effects of Leading Edge Injection on the Film Cooling Characteristics of Multirow Cooling Holes on the Turbine Vane Suction Side Tuijin Jishu/Journal of Propulsion Technology, 2021, 42 (03): : 620 - 629
- [42] Film Cooling Performance of Converging-Slot Holes With Different Exit-Entry Area Ratios JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2011, 133 (01):
- [43] ENHANCEMENT OF FILM COOLING EFFECTIVENESS USING BACKWARD INJECTION HOLES ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2015, VOL 5B, 2015,
- [46] Cooling characteristics of full coverage film holes with opposite lateral ejection angles Hangkong Dongli Xuebao/Journal of Aerospace Power, 2014, 29 (03): : 511 - 518
- [49] A numerical evaluation on the effect of sister holes on film cooling effectiveness and the surrounding flow field Heat and Mass Transfer, 2009, 45 : 1435 - 1446
- [50] FILM COOLING FROM CIRCULAR AND ELLIPTICAL EXIT SHAPED HOLES WITH SISTER HOLE INFLUENCE PROCEEDINGS OF THE ASME TURBO EXPO: TURBINE TECHNICAL CONFERENCE AND EXPOSITION, 2013, VOL 3B, 2013,