共 50 条
- [43] Convective heat transfer through film cooling holes of a gas turbine blade leading edge Proceedings of the ASME Turbo Expo 2005, Vol 3 Pts A and B, 2005, : 833 - 844
- [44] Heat Transfer Coefficient and Film Cooling Effectiveness on the Partial Cavity Tip of a Gas Turbine Blade JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 2019, 141 (07):
- [45] HEAT TRANSFER COEFFICIENT AND FILM COOLING EFFECTIVENESS ON THE PARTIAL CAVITY TIP OF A GAS TURBINE BLADE PROCEEDINGS OF THE ASME TURBO EXPO: TURBOMACHINERY TECHNICAL CONFERENCE AND EXPOSITION, 2018, VOL 5C, 2018, : 379 - 388
- [47] Film cooling with compound angle holes: Heat transfer JOURNAL OF TURBOMACHINERY-TRANSACTIONS OF THE ASME, 1996, 118 (04): : 800 - 806
- [49] Conjugate heat transfer analysis of film cooling flows Journal of Thermal Science, 2006, 15 : 85 - 91
- [50] HEAT TRANSFER AND FILM COOLING OF BLADE TIPS AND ENDWALLS PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 4, PTS A AND B, 2010, : 1763 - 1775