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基于非接触测量技术的低速风洞连续扫描试验技术研究
引用本文:顾艺,岑飞,温渝昌,刘志涛,车兵辉.基于非接触测量技术的低速风洞连续扫描试验技术研究[J].气动实验与测量控制,2013(5):98-104.
作者姓名:顾艺  岑飞  温渝昌  刘志涛  车兵辉
作者单位:中国空气动力研究与发展中心,四川绵阳621000
摘    要:基于Optotrak非接触光学测量系统,建立了风洞试验模型三维姿态角测量方法,实现了模型姿态角的高精度、实时、外触发时钟同步测量。基于该方法测量模型三维实时姿态角,在FL-14低速风洞开展了张线尾撑下YF-16飞机1∶9标模纵、横向连续扫描测力试验。试验结果表明,在0.3°/s的扫描速率下,连续扫描与步进试验数据比对一致性好,各气动分量同期重复性达到国军标合格或先进指标。连续扫描试验获得了更为详尽完整的气动特性信息,同时显著提升了试验效率。

关 键 词:非接触测量  姿态角  连续扫描  Optotrak  风洞试验

Research about continuous scanning test technique based on non-contact measurement technique in low speed wind tunnel
Authors:GU Yi  CEN Fei  WEN Yu-chang  LIU Zhi-tao  CHE Bing-hui
Institution:(China Aerodynamics Research and Development Center, Mianyang Sichuan 621000, China)
Abstract:Based on the non-contact optical measurement system, Optotrak, the authors build the three-dimensional attitude angle measurement method of model in wind tunnel test, and im- plement the high-precision measurement of model attitude angle in real-time and external trigger, clock synchronization mode. 1 : 9 standard model of YF-16 plane's continous scanning test based on measuring attitude angle by Optotrak has been executed in FL-14 low speed wind tunnel. The contrast result shows, under 0.3~/s scan speed, the coincidence indicators between continous scan- ning test and step by step test have achieved the eligible or the advanced index. Compared to step- by-step test, continous scanning test obtains integrated aerodynamic characteristic information and observably upgrades test efficiency.
Keywords:non-contact measurment  attitude angle  continuous scanning  Optotrak  wind tunnel test
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