Aerodynamic modeling and transient performance improvement of a free jet altitude test facility

Feng Wu, Limin Gao, Xinyun Wu, Xudong Feng, Lintao Leng, Yaoyu Li

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

An inlet-engine altitude test facility for flight condition simulation is modeled for the system dynamic performance improvement. The system model equations are solved with an improved Euler integral method. To simulate the interaction between the tested engine and the test bench accurately, a turbojet engine module is introduced in the system model. By modeling and simulation, a linear temperature compensation control algorithm based on the control error is validated for feasibility; controller parameters optimization for cabin static pressure stabilizing is also carried out. In this paper, some issues like temperature transient performance and engine operate impact restraint on cabin static pressure are discussed efficiently and economically. With the characteristics of high efficiency and economy, the modeling and simulation tools are suitable for the optimization of such systems.

源语言英语
主期刊名Artificial Intelligence and Security - 6th International Conference, ICAIS 2020, Proceedings
编辑Xingming Sun, Jinwei Wang, Elisa Bertino
出版商Springer Science and Business Media Deutschland GmbH
618-630
页数13
ISBN(印刷版)9789811581007
DOI
出版状态已出版 - 2020
活动6th International Conference on Artificial Intelligence and Security,ICAIS 2020 - Hohhot, 中国
期限: 17 7月 202020 7月 2020

出版系列

姓名Communications in Computer and Information Science
1254 CCIS
ISSN(印刷版)1865-0929
ISSN(电子版)1865-0937

会议

会议6th International Conference on Artificial Intelligence and Security,ICAIS 2020
国家/地区中国
Hohhot
时期17/07/2020/07/20

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