共 50 条
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- [22] Numerical investigation on aerodynamic loss of turbine cascade with converging slot hole film cooling at suction surface Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2010, 31 (07): : 1312 - 1317
- [23] LEADING-EDGE INJECTION FOR FILM COOLING OF TURBINE VANES JOURNAL OF ENERGY, 1977, 1 (01): : 44 - 49
- [24] Enhancement of film cooling performance at the leading edge of turbine blade PROCEEDINGS OF THE ASME TURBO EXPO 2006, VOL 3, PTS A AND B: HEAT TRANSFER: GENERAL INTEREST, 2006, : 307 - 313
- [29] Numerical studies on film cooling performance of turbine vane leading edge with counter-inclined structure Hangkong Dongli Xuebao, 11 (2609-2618): : 2609 - 2618