Design and Implementation of a Low-Speed Wind Tunnel System

被引:0
|
作者
Zhao, Zheng [1 ]
Zhao, Changchen [3 ]
Pei, Zhongcai [1 ,2 ]
Chen, Weihai [1 ,2 ]
机构
[1] Beihang Univ, Hangzhou Innovat Inst, Hangzhou 310051, Peoples R China
[2] Beihang Univ, Sch Automat Sci & Elect Engn, Beijing 100191, Peoples R China
[3] Zhejiang Univ Technol, Coll Informat Engn, Hangzhou 310051, Peoples R China
基金
浙江省自然科学基金;
关键词
wind tunnel; aerodynamics; measurement and control; system design;
D O I
10.1109/ICIEA51954.2021.9516145
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
Wind tunnel is one of the most important experimental equipment for aerodynamics researches, and most aerodynamic products also need to be tested in wind tunnel before applied in daily life. Most universities and research institutions are actively building wind tunnel laboratories to promote the research of related disciplines. Because of the important position of the wind tunnel system in the field of aerodynamics, many researchers have devoted themselves to wind tunnel design, and modern wind tunnel is developing towards high precision, intelligence, and high reliability. After the investigation of several existing wind tunnel laboratories, this paper designs a low-speed wind tunnel system, which is low cost, high integration, easy to use and maintain, and it can meet the needs of most basic aerodynamics researches.
引用
收藏
页码:273 / 278
页数:6
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