中文版 | English
题名

Aeroacoustic and aerodynamic investigation of multicopter rotors with serrated trailing edges

作者
通讯作者Liu, Yu
DOI
发表日期
2019-05-25
会议名称
The 25th AIAA/CEAS Aeroacoustics Conference
会议录名称
页码
AIAA Paper 2019-2523
会议日期
20-24 May, 2019
会议地点
Delft, Netherlands
出版者
摘要

Multicopters can be observed in many applications, e.g. video taking, mapping, construction, delivery, and rescue operations. In some circumstances, aerodynamic noise of multicopters is a significant concern and quiet rotors would be more competitive in the market. Inspired by owl wings and research of serrations on two-dimensional airfoils, trailing edge serrations are adopted for noise reduction of three-dimensional multicopter rotors. By choosing different parameters of serrations, i.e. height to wave-length ratio ( ) and retrofitted manner of add-on and cut-in, noise reduction and aerodynamic performance of different rotors are compared at forward flight conditions. The add-on serration rotors generate higher thrust than cut-in serration ones for the same rotation speed. The serration parameter of performs the best among different designs in terms of overall sound pressure level decrease at the same thrust. Broadband noise decrease in the middle to high frequency range is observed for all designs, but it is less significant in comparison with rotor tonal noise, and the rotor noise decrease is mainly a result of the improved aerodynamic performance.
© 2019, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.

学校署名
第一 ; 通讯
语种
英语
收录类别
资助项目
National Natural Science Foundation of China[11602290]
EI入藏号
20195107868770
EI主题词
Acoustic Noise ; Aerodynamics ; Noise Abatement
EI分类号
Aerodynamics, General:651.1 ; Acoustics, Noise. Sound:751 ; Acoustic Noise:751.4
来源库
EV Compendex
引用统计
被引频次[WOS]:0
成果类型会议论文
条目标识符http://sustech.caswiz.com/handle/2SGJ60CL/50967
专题工学院_力学与航空航天工程系
作者单位
1.Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology, Shenzhen, Guangdong 518055, China
2.Key Laboratory of Aerodynamic Noise Control, China Aerodynamics Research and Development Center, Mianyang, Sichuan 621000, China
第一作者单位力学与航空航天工程系
通讯作者单位力学与航空航天工程系
第一作者的第一单位力学与航空航天工程系
推荐引用方式
GB/T 7714
Yang, Yannian,Li, Yu,Liu, Yu,et al. Aeroacoustic and aerodynamic investigation of multicopter rotors with serrated trailing edges[C]:American Institute of Aeronautics and Astronautics (AIAA),2019:AIAA Paper 2019-2523.
条目包含的文件
条目无相关文件。
个性服务
原文链接
推荐该条目
保存到收藏夹
查看访问统计
导出为Endnote文件
导出为Excel格式
导出为Csv格式
Altmetrics Score
谷歌学术
谷歌学术中相似的文章
[Yang, Yannian]的文章
[Li, Yu]的文章
[Liu, Yu]的文章
百度学术
百度学术中相似的文章
[Yang, Yannian]的文章
[Li, Yu]的文章
[Liu, Yu]的文章
必应学术
必应学术中相似的文章
[Yang, Yannian]的文章
[Li, Yu]的文章
[Liu, Yu]的文章
相关权益政策
暂无数据
收藏/分享
所有评论 (0)
[发表评论/异议/意见]
暂无评论

除非特别说明,本系统中所有内容都受版权保护,并保留所有权利。