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Wind Tunnel Strain-Gage Balance Calibration Data Analysis Using a Weighted Least Squares ApproachA new approach is presented that uses a weighted least squares fit to analyze wind tunnel strain-gage balance calibration data. The weighted least squares fit is specifically designed to increase the influence of single-component loadings during the regression analysis. The weighted least squares fit also reduces the impact of calibration load schedule asymmetries on the predicted primary sensitivities of the balance gages. A weighting factor between zero and one is assigned to each calibration data point that depends on a simple count of its intentionally loaded load components or gages. The greater the number of a data point's intentionally loaded load components or gages is, the smaller its weighting factor becomes. The proposed approach is applicable to both the Iterative and Non-Iterative Methods that are used for the analysis of strain-gage balance calibration data in the aerospace testing community. The Iterative Method uses a reasonable estimate of the tare corrected load set as input for the determination of the weighting factors. The Non-Iterative Method, on the other hand, uses gage output differences relative to the natural zeros as input for the determination of the weighting factors. Machine calibration data of a six-component force balance is used to illustrate benefits of the proposed weighted least squares fit. In addition, a detailed derivation of the PRESS residuals associated with a weighted least squares fit is given in the appendices of the paper as this information could not be found in the literature. These PRESS residuals may be needed to evaluate the predictive capabilities of the final regression models that result from a weighted least squares fit of the balance calibration data.
Document ID
20170005257
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Ulbrich, N.
(Jacobs Technology, Inc. Moffett Field, CA, United States)
Volden, T.
(Jacobs Technology, Inc. Moffett Field, CA, United States)
Date Acquired
June 7, 2017
Publication Date
June 5, 2017
Subject Category
Numerical Analysis
Research And Support Facilities (Air)
Report/Patent Number
ARC-E-DAA-TN41575
Report Number: ARC-E-DAA-TN41575
Meeting Information
Meeting: AIAA AVIATION Forum 2017
Location: Denver, CO
Country: United States
Start Date: June 5, 2017
End Date: June 9, 2017
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA16BD26C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
calibration analysis
wind tunnel balance
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