【Key words】 turbine cascade； aerodynamic characteristic； clearance size；
基于14个网页-相关网页
Firstly, the paper investigates a turbine cascade with two rows of slots in leading edge and a turbine cascade with two rows of straight/inclined holes in leading edge based on the experiment through the Fine/Turbo software.
本文以一个涡轮叶栅气膜冷却实验模型为研究对象,采用Fine/Turbo软件包,分别对一个叶片前缘开有两道槽缝和两个叶片前缘开有直/斜孔的模型进行了数值模拟。
参考来源 - 涡轮叶栅气膜冷却流场的数值研究·2,447,543篇论文数据，部分数据来源于NoteExpress
给出了一个计算亚、跨音涡轮叶栅叶型损失的数值计算方法。
A new numerical method for predicting the profile loss of turbine blades in subsonic and supersonic flows is presented.
为论证方法的有效性，给出了几个跨音速涡轮叶栅的计算结果。
Several computed results of transonic turbine cascades are presented to illustrate the method's capabilities.
详细测量了平行进口端壁附面层与设前导叶两种进口条件下某涡轮叶栅的出口流场。
The exit flow fields of a turbine cascade with or without the front guide vanes were investigated.
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