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风洞试验中模型迎角视觉测量技术研究
引用本文:孙岩,张征宇,黄诗捷,喻波,王水亮. 风洞试验中模型迎角视觉测量技术研究[J]. 航空学报, 2013, 34(1): 1-7. DOI: 10.7527/S1000-6893.2013.0001
作者姓名:孙岩  张征宇  黄诗捷  喻波  王水亮
作者单位:1. 中国空气动力研究与发展中心空气动力学国家重点实验室,四川绵阳,621000
2. 中国空气动力研究与发展中心空气动力学国家重点实验室,四川绵阳 621000;西南科技大学信息工程学院,四川绵阳 621000
3. 西南科技大学信息工程学院,四川绵阳,621000
基金项目:国家自然科学基金(51075385);国家“973”计划(2009CB723801)~~
摘    要: 发展了一种基于双相机的风洞试验模型迎角视觉测量技术。即在风洞模型表面绘制或喷涂一些高对比度的标记点,采用两台400万像素的工业相机采集模型的运动图像,然后求解图像的共线方程获得模型表面标记点的三维空间坐标,利用表面标记点坐标最小二乘拟合出一条空间直线,通过不同时刻空间直线单位方向矢量的变化计算出模型的迎角变化。利用精密电子倾斜仪对迎角视觉测量系统进行静态标定,结果表明:迎角视觉测量系统的准确度在0.01°以内。迎角视觉测量系统在2 m超声速风洞中对一尾支撑无主测力天平铰链力矩测量模型的实时迎角进行了测量,结果表明:系统具有很好的响应特性,可以作为风洞试验中迎角测量的一种有效方法,尤其是用于无主测力天平时模型真实迎角和支杆弹性角的测量。

关 键 词:风洞试验  迎角  视觉测量  主测力天平  支杆弹性角  
收稿时间:2012-02-17;

Vision Measurement Technology Research for Model Angle of Attack in Wind Tunnel Tests
SUN Yan , ZHANG Zhengyu , HUANG Shijie , YU Bo , WANG Shuiliang. Vision Measurement Technology Research for Model Angle of Attack in Wind Tunnel Tests[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(1): 1-7. DOI: 10.7527/S1000-6893.2013.0001
Authors:SUN Yan    ZHANG Zhengyu    HUANG Shijie    YU Bo    WANG Shuiliang
Affiliation:1.State Key Laboratory of Aerodynamics,China Aerodynamics Research and Development Center, Mianyang 621000,China 2.Information Engineering College,Southwest University of Science and Technology,Mianyang 621000,China
Abstract:A vision measuring technique based on two cameras is developed to measure model angles of attack in wind tunnel tests. Two high-speed industrial cameras with 4 million pixels are used to capture the motion images of the tested model, on the surface of which some high contrast targets are painted. Then the three-dimensional coordinates of the targets are acquired by the solution of the imaging collinear equations. The changes of angle of attack are calculated through the change of the unit vectors of the space lines fitted by the three-dimensional coordinates of the targets. Static validation results on the angle of attack vision measurement system by sophisticated electronic clinometer indicate that the accuracy of the angle of attack vision measurement system is within 0.01°. Dynamic test results on a hinge moment measuring model which is fixed on a sting without main load balance in a 2 m supersonic wind tunnel indicate that the measurement system has good response characteristics and can be used as an effective method for measurement of angle of attack in a high speed wind tunnel, especially for measurement of accurate angle of attack of models and sting elastic angle with the absence of a main load balance.
Keywords:wind tunnel test  angle of attack  vision measurement  main load balance  sting elastic angle
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