共 50 条
- [22] Application of local indentations for film cooling of gas turbine blade leading edge Thermophysics and Aeromechanics, 2016, 23 : 713 - 720
- [24] Experimental study on film cooling of turbine blade leading edge in deposition environment Beijing Hangkong Hangtian Daxue Xuebao/Journal of Beijing University of Aeronautics and Astronautics, 2021, 47 (11): : 2189 - 2199
- [27] Effect of the Injection Angle on the Leading Edge Film Cooling of a Rotating Turbine Blade 1600, Science Press (41): : 320 - 328
- [29] Film cooling with compound angle holes in leading edge of twisted turbine blade Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2023, 44 (18):