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Improved Regression Analysis of Temperature-Dependent Strain-Gage Balance Calibration Data

机译:改进了温度相关的应变计量平衡校准数据的回归分析

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An improved approach is discussed that may be used to directly include first and second order temperature effects in the load prediction algorithm of a wind tunnel strain-gage balance. The improved approach was designed for the Iterative Method that fits strain-gage outputs as a function of calibration loads and uses a load iteration scheme during the wind tunnel test to predict loads from measured gage outputs. The improved approach assumes that the strain-gage balance is at a constant uniform temperature when it is calibrated and used. First, the method introduces a new independent variable for the regression analysis of the balance calibration data. The new variable is defined as the difference between the uniform temperature of the balance and a global reference temperature. This reference temperature should be the primary calibration temperature of the balance so that, if needed, a tare load iteration can be performed. Then, two temperature-dependent terms are included in the regression models of the gage outputs. They are the temperature difference itself and the square of the temperature difference. Simulated temperature-dependent data obtained from Triumph Aerospace's 2013 calibration of NASA's ARC-30K five-component semi-span balance is used to illustrate the application of the improved approach.
机译:讨论了一种可以用于直接包括在风隧道应变计平衡的负载预测算法中的第一和二阶温度效应的改进的方法。改进的方法是为迭代方法设计的,该方法适合应变计输出作为校准负载的函数,并且在风隧道测试期间使用负载迭代方案来预测来自测量的量输出的负载。改进的方法假设当校准并使用时,应变计平衡在恒定的均匀温度下。首先,该方法引入了一个新的独立变量,用于对平衡校准数据的回归分析。新变量定义为余量均匀温度与全局参考温度之间的差异。该参考温度应该是余量的主要校准温度,因此如果需要,可以执行皮重迭代。然后,在量输出的回归模型中包括两个温度相关的术语。它们是温差本身和温差平方。从凯旋航空航天2013年校准NASA的ARC-30K五分量半跨度平衡的模拟温度依赖数据用于说明改进方法的应用。

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