北京航空航天大学主页平台系统张伟昊--中文主页-- Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance

扫描手机二维码

欢迎您的访问
您是第位访客

开通时间：..

最后更新时间：..

论文当前位置：中文主页 >> 论文

Dominant flow structure in the squealer tip gap and its impact on turbine aerodynamic performance

点击次数：
合写作者： et al., Zhang W.*, Li Y., F., Shao, Z.*,Zou
是否译文：否

上一条： Experimental investigation on the effects of wake passing frequency on boundary layer transition in high-lift low-pressure turbines

下一条： Impact of stagger angle nonuniformity on turbine aerodynamic performance