An integrated modeling approach for variable cycle engine performance analysis

被引:6
|
作者
Zhang, Xiaobo [1 ]
Wang, Zhanxue [1 ]
Zhou, Li [1 ]
机构
[1] Northwestern Polytech Univ, Sch Power & Energy, Shaanxi Key Lab Internal Aerodynam Aeroengine, Xian 710072, Peoples R China
基金
中国国家自然科学基金;
关键词
SIMULATION;
D O I
10.1016/j.jfranklin.2023.03.013
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The present study aims to address the issue of accuracy degradation in the traditional zero -dimensional variable cycle engine (VCE) model due to the multi-angle characteristics in the core driven fan stage (CDFS). To this end, a two-dimensional model was established through the application of the streamline curvature method. Subsequently, a multi-level VCE model was developed incorporating three zooming strategies to integrate the CDFS characteristics. The simulation results reveal that the proposed multi-level modeling approach is relatively time-efficient, requiring only half the computational time of fully coupled strategies. The results indicate a significant improvement in terms of optimal thrust and specific fuel consumption (sfc) when compared to the traditional zero-dimensional VCE model, with differences in maximum thrust and sfc of 3 . 11% and 1 . 24% , respectively. Furthermore, the average time required to solve one working point remains less than one second.(c) 2023 The Franklin Institute. Published by Elsevier Inc. All rights reserved.
引用
收藏
页码:5549 / 5563
页数:15
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