Installation Characteristics of Variable Cycle Engine Based on Inlet Flow Matching

被引:8
作者
Chen, Haoying [1 ]
Zhang, Haibo [1 ]
Wang, Yong [1 ]
Zhen, Qiangang [1 ]
机构
[1] Nanjing Univ Aeronaut & Astronaut, Coll Energy & Power Engn, Jiangsu Prov Key Lab Aerosp Power Syst, 29 Yudao St, Nanjing 210016, Peoples R China
基金
中国国家自然科学基金;
关键词
variable cycle engine; inlet; varying geometry components; spillage drag; the installation performance;
D O I
10.1515/tjj-2018-0031
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
As per few investigation in installed performance for variable cycle engines, an analysis scheme is proposed on the basis of integrating variable cycle engine and supersonic inlet system model. An integrated mathematical model, containing the inlet and the variable cycle engine is built, realizing the simulation of influences on the installation performance by varying geometry components. The impact on engine performance of variable geometric regulation was analyzed and concluded respectively. The experimental results show that the overflow resistance of the variable cycle engine with variable geometry optimization is reduced at subsonic cruise stage, and the installed fuel consumption is reduced, which significantly improves the installation performance.
引用
收藏
页码:319 / 329
页数:11
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