当前位置: X-MOL 学术Proc. Inst. Mech. Eng. Part G J. Aerosp. Eng. › 论文详情
Our official English website, www.x-mol.net, welcomes your feedback! (Note: you will need to create a separate account there.)
Performance improvement of a high-speed aero-fuel centrifugal pump through active inlet injector
Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering ( IF 1.0 ) Pub Date : 2020-09-23 , DOI: 10.1177/0954410020960961
Jia Li 1 , Xin Wang 1 , Wancheng Wang 2 , Yue Wang 2
Affiliation  

This paper presents a high-speed aero-fuel centrifugal pump with an active inlet injector for an aero-engine aiming at regulating the internal flow field and improving overall hydraulic performance...

中文翻译:

通过主动进气喷射器提高高速航空燃油离心泵的性能

本文提出了一种用于航空发动机的带有主动进气喷射器的高速航空燃料离心泵,旨在调节内部流场并提高整体水力性能...
更新日期:2020-09-23
down
wechat
bug