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Analysis of coupling effects between flight and propulsion systems for DPC aircraft

  • Beijing Institute of Control and Electronic Technology

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

The noteworthy feature of aircraft with distribute propulsion configuration is the integration of the fuselage and semi-embedded distributed propulsion system, which brings strong coupling effects between flight and propulsion systems. The aim of this article is to systematically investigate the coupling effects due to boundary layer ingestion under different flight states. As the basis, the definition of boundary layer ingestion is put forward and the modeling process of distributed propulsion system is described in detail. An analysis method based on the distributed propulsion model and CFD computation is proposed. By using this method, the coupling characteristics between flight and propulsion system are generally analyzed under different flight heights and velocities. The results of this study demonstrate that the coupling effects can significantly improve the aerodynamic performance.

源语言英语
主期刊名Proceedings of the 2016 12th World Congress on Intelligent Control and Automation, WCICA 2016
出版商Institute of Electrical and Electronics Engineers Inc.
1653-1657
页数5
ISBN(电子版)9781467384148
DOI
出版状态已出版 - 27 9月 2016
活动12th World Congress on Intelligent Control and Automation, WCICA 2016 - Guilin, 中国
期限: 12 6月 201615 6月 2016

出版系列

姓名Proceedings of the World Congress on Intelligent Control and Automation (WCICA)
2016-September

会议

会议12th World Congress on Intelligent Control and Automation, WCICA 2016
国家/地区中国
Guilin
时期12/06/1615/06/16

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