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

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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%.

Original languageEnglish
Title of host publication2018 Joint Propulsion Conference
PublisherAmerican Institute of Aeronautics and Astronautics Inc, AIAA
ISBN (Print)9781624105708
DOIs
StatePublished - 2018
Event54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018 - Cincinnati, United States
Duration: 9 Jul 201811 Jul 2018

Publication series

Name2018 Joint Propulsion Conference

Conference

Conference54th AIAA/SAE/ASEE Joint Propulsion Conference, 2018
Country/TerritoryUnited States
CityCincinnati
Period9/07/1811/07/18

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