Numerical analysis on the flow characteristics of rotating axial orifices under non-rotation method

Jiajia Niu, Gaowen Liu, Qing Feng, Cunliang Liu, Li Zhou, Heng Wu

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

As an important throttling component in the engine internal cooling system, rotating orifices are widely used in rotating parts like turbine disks, drums, shafts and so on. Considering the difficulty in carrying out the experiment and measurement, a non-rotation method to measure the discharge coefficient of an rotating axial orifice was presented in this paper. Numerical simulation was conducted to study the difference of flow characteristics between rotation method and non-rotation method as well as the influence of the incidence angle in the range of 0°-70°. Results show that: within the range of parameters studied, the distributions of relative total velocity and relative total pressure using non-rotation method are quite similar to those under rotation method. The deviation of relative total velocity between the two methods is less than 5%. The deviation of relative total pressure is less than 0.5%, and that of discharge coefficient is less than 3.54%.

源语言英语
主期刊名2018 Joint Propulsion Conference
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105708
DOI
出版状态已出版 - 2018
活动54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018 - Cincinnati, 美国
期限: 9 7月 201811 7月 2018

出版系列

姓名2018 Joint Propulsion Conference

会议

会议54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
国家/地区美国
Cincinnati
时期9/07/1811/07/18

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