位置：成果数据库 > 期刊 > 期刊详情页
The Effects of Trailing Edge Thickness on the Losses of Ultrahigh Lift Low Pressure Turbine Blades
  • ISSN号：0889-504X
  • 期刊名称：Journal of Turbomachinery
  • 时间：2014.8
  • 页码：-
  • 相关项目：叶尖小翼对涡轮叶片叶尖泄漏流气动性能作用机理的研究
作者： Zhou, Chao|Hodson, Howard|Himmel, Christoph|
同期刊论文项目
叶尖小翼对涡轮叶片叶尖泄漏流气动性能作用机理的研究
期刊论文 11
同项目期刊论文
Aerodynamic performance of tip leakage flow of two different blade tips in transonic turbine
跨声速条件下气膜冷却对平面叶尖流动和传热特性的影响
跨声速叶栅中气膜冷却对平面叶尖流动和传热特性的影响
Aerothermal Performance of Different Tips in Transonic Turbine Cascade with End-Wall Motion
Effect of film cooling on flow and heat transfer of flat tip in transonic turbine cascade
Effects of Winglet Geometry on the Aerodynamic Performance of Tip Leakage Flow in a Turbine Cascade
Effects of endwall motion on thermal performance of cavity tips with different squealer width and he
The effects of trailing edge thickness on the losses of ultra-high lift LP turbine blades
Thermal Performance of Transonic Cooled Tips in a Turbine Cascade
跨声速涡轮中两种叶片叶尖泄漏流的气动性能