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The Effects of Inlet Reynolds Number, Exit Mach Number and Incidence Angle on Leading Edge Film Cooling Effectiveness of a Turbine Blade in a Linear Transonic Cascade 会议论文
ASME, 2015
作者:  Cong Liu;  Hui-ren Zhu;  Zhong-yi Fu;  Run-hong Xu
收藏  |  浏览/下载:20/0  |  提交时间:2016/01/25
Effect of Incidence Angle on Gas Turbine First-Stage Nozzle Guide Vane Leading Edge and Gill Region Film Cooling 会议论文
ASME, Copenhagen, Denmark, 41071
Yang Zhang; Xin Yuan
收藏  |  浏览/下载:11/0  |  提交时间:2012/08/10
Film Cooling Effectiveness Distribution on First-Stage Vane Endwall With and Without Leading-Edge Fillets: Part II—Effect of Incidence Angle 会议论文
ASME, Vancouver, British Columbia, Canada, 2011-06-06
Yang Zhang; Xin Yuan
收藏  |  浏览/下载:8/0  |  提交时间:2012/07/18


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