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风洞模型激光攻角测量 被引量:2

Laser Measurement of Attack Angle by Wind- tunnel Model
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摘要 给出一种用于风洞飞机模型攻角测量的方法.采用对称双光束交叠照射角传感器,风洞实验测角范围由40°增加到76°;利用电子处理器计数干涉条纹,测角精度可达0.005°. A method for measuring attack angle by wind-tunnel model is described. By using laser angle senser (LAS) with two symmetrical and overlapping beams, the angle measured in dynamic state is increased from 40 ° to 76° . Whereas, the error in angle measurement is reduced to 0.005° .
出处 《大连铁道学院学报》 2002年第3期46-48,共3页 Journal of Dalian Railway Institute
关键词 风洞模型 攻角测量 飞机模型 对称双光束交叠照射角传感器 laser interference measurement attack angle
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参考文献1

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同被引文献24

  • 1张孝棣,蒋甲利,贾元胜,马洪志,肖亚克.视频测量方法在风洞模型姿态角测量中的应用[J].实验流体力学,2005,19(3):21-25. 被引量:12
  • 2恽起麟.风洞实验数据的误差与修正[M].北京:国防工业出版社,1996..
  • 3王瑞波,李平,谢艳,杨可,钟世东.攻角传感器在2.4m跨声速风洞中的应用[J].兵工自动化,2007,26(7):80-81. 被引量:3
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  • 7Jones T W, Hoppe J C. Comparison of angle of attack measurements for wind tunnel testing. 39th AIAA Aero- space Sciences Meeting & Exhibit, 2001.
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