共 50 条
- [2] Experimental Study of Heat Transfer Augmentation Near the Entrance to a Film Cooling Hole in a Turbine Blade Cooling Passage [J]. JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2009, 131 (04): : 1 - 11
- [3] Rotating effects on heat transfer rate in a cooling air passage of a gas turbine blade [J]. PROCEEDINGS OF 2004 ASME POWER, 2004, : 237 - 242
- [4] Experimental study on the heat transfer in the compound cooling passage [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 3, PTS A AND B: HEAT TRANSFER: GENERAL INTEREST, 2006, : 241 - 247
- [5] NUMERICAL INVESTIGATION OF FLUID FLOW AND HEAT TRANSFER IN A TURBINE BLADE WITH SERPENTINE PASSAGE AND LATTICEWORK COOLING [J]. PROCEEDINGS OF THE ASME TURBO EXPO 2008, VOL 4, PTS A AND B, 2008, : 383 - 391
- [6] Experimental investigation of film cooling heat transfer on turbine blade leading edge [J]. Tuijin Jishu, 2 (64-68):
- [9] Experimental investigation of heat transfer and flow using V and broken V ribs within gas turbine blade cooling passage [J]. Heat and Mass Transfer, 2015, 51 : 631 - 647