Experimental Investigation on Film Cooling Characteristics of Conical Holes on a Turbine Blade Tip in Transonic Flow

被引：0
|
作者：
Zhang, Bo-Lun [1 ,2 ]
Xia, Jun [1 ]
Shen, Zhi-Qiang [1 ]
Zhu, Hui-Ren [2 ]
机构：
[1] College of Aerospace Science and Engineering, National University of Defense Technology, Changsha,410072, China
[2] School of Power and Energy, Northwestern Polytechnical University, Xi’an,710072, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2023年 / 44卷 / 08期
关键词：
Engineering Village;
D O I：
22010014
中图分类号：
学科分类号：
摘要：
Blade tip - Density ratio - Experimental investigations - Film cooling - Film cooling effectiveness - Film-cooling characteristics - Mass flow ratios - Pressure sensitive paint technique - Squealer tip - Turbine blade tip
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