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用于低速风洞飞行器气动导数试验的绳牵引并联支撑系统
引用本文:郑亚青,林麒,刘雄伟.用于低速风洞飞行器气动导数试验的绳牵引并联支撑系统[J].航空学报,2009,30(8):1549-1554.
作者姓名:郑亚青  林麒  刘雄伟
作者单位:1. 厦门大学,物理与机电工程学院,福建,厦门,361005;华侨大学,机电及自动化学院,福建,泉州,362021
2. 厦门大学,物理与机电工程学院,福建,厦门,361005
3. 中央兰开夏大学,计算、工程与物理科学学院,英国,普雷斯顿,PR1 2HE
4. 法国国家科学研究中心,G-SCOP实验室,法国,格勒诺布尔,38031
基金项目:国家自然科学基金(50475099);;福建省青年科技人才创新基金(2006F3083)
摘    要: 为了用同一套绳牵引并联支撑系统来实现低速风洞静导数和动导数实验,采用理论与实验相结合的方法,总结了在WDPSS-8项目中所做的研究工作。结果表明,传统的杆支撑系统存在如支架对空气流场的影响等不可避免的缺陷;张线支撑系统很适合用于飞行器的静导数实验中,但它不能用在飞行器的动导数实验中;绳牵引并联支撑系统WDPSS-8能成功用于静导数实验中,且它在动导数实验中有潜在用途。WDPSS-8项目中的理论问题都得到解决,但实验方面还有不少问题有待解决。

关 键 词:风洞  支撑系统  绳牵引  静导数  动导数  

On Wire-driven Parallel Suspension Systems for Static and Dynamic Derivatives of Aircraft in Low-speed Wind Tunnels
Zheng Yaqing,Lin Qi,Liu Xiongwei,Mitrouchev Peter.On Wire-driven Parallel Suspension Systems for Static and Dynamic Derivatives of Aircraft in Low-speed Wind Tunnels[J].Acta Aeronautica et Astronautica Sinica,2009,30(8):1549-1554.
Authors:Zheng Yaqing  Lin Qi  Liu Xiongwei  Mitrouchev Peter
Institution:1.School of Physics and Mechanical and Electrical Engineering;Xiamen University;Xiamen 361005;China;2.College of Mechanical Engineering and Automation;Huaqiao University;Quanzhou 362021;China;3.School of Computing;Engineering and Physical Sciences;University of Central Lancashire;Preston PR1 2HE;UK;4.G-SCOP Laboratory;French National Center for Scientific Research;Grenoble 38031;France
Abstract:In order to use the same wire-driven parallel suspension system to implement static and dynamic derivative experiments in low-speed wind tunnels,a survey of the research work addressing the wire-driven parallel suspension system with eight wires(WDPSS-8) projects is presented in this article.The research methodology combines both theoretical and experimental aspects.The results show that,there are some unavoidable drawbacks,such as the interference of the streamline flow brought by the strut in the traditio...
Keywords:wind tunnel  suspension system  wire-driven  static derivative  dynamic derivative  
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