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Analysis of Sting Balance Calibration Data Using Optimized Regression ModelsCalibration data of a wind tunnel sting balance was processed using a candidate math model search algorithm that recommends an optimized regression model for the data analysis. During the calibration the normal force and the moment at the balance moment center were selected as independent calibration variables. The sting balance itself had two moment gages. Therefore, after analyzing the connection between calibration loads and gage outputs, it was decided to choose the difference and the sum of the gage outputs as the two responses that best describe the behavior of the balance. The math model search algorithm was applied to these two responses. An optimized regression model was obtained for each response. Classical strain gage balance load transformations and the equations of the deflection of a cantilever beam under load are used to show that the search algorithm s two optimized regression models are supported by a theoretical analysis of the relationship between the applied calibration loads and the measured gage outputs. The analysis of the sting balance calibration data set is a rare example of a situation when terms of a regression model of a balance can directly be derived from first principles of physics. In addition, it is interesting to note that the search algorithm recommended the correct regression model term combinations using only a set of statistical quality metrics that were applied to the experimental data during the algorithm s term selection process.
Document ID
20100024136
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Ulbrich, N.
(Jacobs Technology, Inc. Moffett Field, CA, United States)
Bader, Jon B.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 24, 2013
Publication Date
August 2, 2010
Subject Category
Numerical Analysis
Report/Patent Number
ARC-E-DAA-TN712
AIAA Paper 2009-5372
Report Number: ARC-E-DAA-TN712
Report Number: AIAA Paper 2009-5372
Meeting Information
Meeting: 45th AIAAfASME/SAEfASEE Joint Propulsion Conference
Location: Denver, CO
Country: United States
Start Date: August 2, 2008
End Date: August 5, 2008
Sponsors: American Inst. of Aeronautics and Astronautics, American Society for Electrical Engineers, Society of Automotive Engineers, Inc., American Society of Mechanical Engineers
Funding Number(s)
CONTRACT_GRANT: NNA04BA85C
Distribution Limits
Public
Copyright
Public Use Permitted.
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