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MEASUREMENT METHOD FOR DYNAMIC POSITION OF AEROFOIL BASE LINE BASED ON IFEM AND RZT

机译:基于IFEM和RZT的翼型线动态位置测量方法。

摘要

The present invention discloses a measurement method for the dynamic position of aerofoil base line based on iFEM (Inverse Finite Element Method) and RZT (Refined Zigzag Theory). The method comprises four steps: determining the three-dimensional model of the selected aerofoil; designing the FBG (Fiber Bragg Grating) sensor array and the layout design of strain rosette on aerofoil surface; establishing an adverse-finite element simulation model based on RZT theory; reading and converting the measurement data to obtain the dynamic position of aerofoil base line. The present invention realizes a measurement method for the dynamic position of aerofoil base line based on RZT, which has good robustness and adaptability.
机译:本发明公开了一种基于iFEM(逆有限元法)和RZT(精细之字形理论)的翼型基线动态位置的测量方法。该方法包括四个步骤:确定所选翼型的三维模型;设计FBG(光纤布拉格光栅)传感器阵列以及翼型表面上应变花环的布局设计;基于RZT理论建立逆向有限元仿真模型;读取并转换测量数据以获得机翼基线的动态位置。本发明实现了一种基于RZT的翼型基线动态位置测量方法,具有很好的鲁棒性和适应性。

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