Research on film cooling performance of sister hole based on structural parameter analysis

被引：0
|
作者：
Wang J. [1 ]
Sun J. [1 ]
Zhao Z. [1 ]
Zhang B. [1 ]
Ren X. [2 ,3 ]
Xie G. [4 ]
机构：
[1] School of Energy and Environmental Engineering, Hebei University of Technology, Tianjin
[2] Key Laboratory for Thermal Science and Power Engineering of Ministry of Education, Tsinghua University, Beijing
[3] Collaborative Innovation Center for Advanced Aero-Engine, Beijing
[4] School of Marine Science and Technology, Northwestern Polytechnical University, Xi'an
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2021年 / 42卷 / 07期
基金：
中国国家自然科学基金;
关键词：
Blowing ratio; Compound angle; Film cooling effectiveness; Sister holes; Taguchi method;
D O I：
10.7527/S1000-6893.2020.24775
中图分类号：
学科分类号：
摘要：
A three-factor and five-level orthogonal table is designed using the Taguchi method for the sister hole structure, with the compound angle, the inclination angle and the blowing ratio as factors and the average wall film cooling effectiveness as the evaluation index. The flow characteristics and the cooling effectiveness distribution under different conditions are analyzed with numerical calculations. Results show that the film cooling effectiveness of the sister holes is 165%-412.5% of that of conventional cylindrical holes at a high blowing ratio, and the film cooling effectiveness of the sister holes with a 10° compound angle is higher than that of the sister holes with a -10° compound angle. Parameterized results reveal that the hole structure with a blowing ratio of 0.5, a compound angle of 10° and an inclination angle of 35° exhibits the best cooling performance. © 2021, Beihang University Aerospace Knowledge Press. All right reserved.
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