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Wind Tunnel Investigation of Aeroelasticity on an Elastic Wing Coupled with Propeller Effects

  • Beihang University
  • China Research and Development Academy of Machinery Equipment
  • Technology CO.LTD

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

This paper investigates the aeroelasticity of an elastic wing coupled with propeller effects as compared to rigid counterparts by conducting a wind tunnel experiment specifically tailored for the propeller/wing system, examining the variation in wing deformation and lift contribution rates due to the propeller effects. The empirical data derived from the experiment underscore the necessity of accounting for the characteristics of aeroelasticity in an elastic wing coupled with propeller effects, offering valuable engineering insights for the design and computational simulation of propeller-equipped aircraft.

源语言英语
主期刊名Mechanical and Aerospace Engineering - Proceedings of the 15th International Conference, ICMAE 2024
编辑Pasquale Daponte
出版商IOS Press BV
582-589
页数8
ISBN(电子版)9781643685984
DOI
出版状态已出版 - 16 6月 2025
活动15th International Conference on Mechanical and Aerospace Engineering, ICMAE 2024 - Zagreb, 克罗地亚
期限: 17 7月 202420 7月 2024

出版系列

姓名Advances in Transdisciplinary Engineering
71
ISSN(印刷版)2352-751X
ISSN(电子版)2352-7528

会议

会议15th International Conference on Mechanical and Aerospace Engineering, ICMAE 2024
国家/地区克罗地亚
Zagreb
时期17/07/2420/07/24

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