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SENSOR TYPE WIND EXPERIMENTAL MODEL SETTING SYSTEM

机译:传感器式风实验模型设置系统

摘要

The present invention relates to a sensor type wind tunnel test model setting system. The sensor type wind tunnel test model setting system includes: a contactless distance measurement sensor (20) generating a transmitting and receiving signal to detect data on a posture angle (an attack angle, a reentering angle, and a roll angle) of a wind tunnel test model (100) installed in a wind tunnel test space; a signal processing module (30) extracting distance information of the wind tunnel test model (100) from the data on the posture angle of the contactless distance measurement sensor (20); and a distance information analysis module (40) providing correction data to improve accuracy of the posture angle by analyzing the posture angle of the wind tunnel test model (100). The posture angle of the wind tunnel test model (100), which should be measured by the contactless distance measurement sensor (20) based on a rotation center axis, is accurately set. Aerodynamic data of a wing deformed due to aerodynamics can be accurately obtained since a wind tunnel test is performed in a similar test condition as an actual flight condition by setting the accurate posture angle.
机译:本发明涉及一种传感器式风洞测试模型设置系统。传感器式风洞测试模型设定系统包括:非接触式测距传感器(20),该传感器产生发送和接收信号以检测关于风洞的姿态角(迎角,再进入角和侧倾角)的数据。安装在风洞测试空间中的测试模型(100);信号处理模块(30)从与非接触式测距传感器(20)的姿态角有关的数据中提取风洞测试模型(100)的距离信息;距离信息分析模块(40)提供校正数据,以通过分析风洞测试模型(100)的姿态角来提高姿态角的准确性。准确地设定风洞测试模型(100)的姿势角,该姿势角应由非接触式距离测量传感器(20)基于旋转中心轴来测量。由于通过设置精确的姿势角,在与实际飞行条件相似的测试条件下进行风洞测试,因此可以精确地获得由于空气动力学而变形的机翼的空气动力学数据。

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