Active Flow Control Method for Small Ducted Aircraft

Yan xuan Wu, Xiao yu Qiao*, Xin yue Zhao, Wei Zhang

*此作品的通讯作者

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

The small ducted type aircraft adopts the control rudder surface as the main flight attitude control surface of the aircraft. In order to produce enough control torque in the limited space, the control rudder surface needs to be completely located in the under wash flow of the culvert fan. Therefore, the control rudder is generally installed in the culvert ring, located below the fan. The rudder deflection produces a control torque to tilt the aircraft, and the high-speed level flight of the aircraft is realized by the forward component of engine thrust/pull force. This control method is deficient caused by the flow characteristics of the culvert around the stream. Therefore, the active flow control scheme based on synthetic jet is used to control the position of air separation artificially to help the control rudder surface to produce enough and stable control torque. The steady jet and synthetic jet are analyzed and verified by CFD simulation method, and a lot of data are obtained. This paper provides a new idea for the development of small ducted aircraft control system in the future.

源语言英语
主期刊名Proceedings of 2021 International Conference on Autonomous Unmanned Systems, ICAUS 2021
编辑Meiping Wu, Yifeng Niu, Mancang Gu, Jin Cheng
出版商Springer Science and Business Media Deutschland GmbH
2318-2326
页数9
ISBN(印刷版)9789811694912
DOI
出版状态已出版 - 2022
活动International Conference on Autonomous Unmanned Systems, ICAUS 2021 - Changsha, 中国
期限: 24 9月 202126 9月 2021

出版系列

姓名Lecture Notes in Electrical Engineering
861 LNEE
ISSN(印刷版)1876-1100
ISSN(电子版)1876-1119

会议

会议International Conference on Autonomous Unmanned Systems, ICAUS 2021
国家/地区中国
Changsha
时期24/09/2126/09/21

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