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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 search algorithm that identifies an optimized regression model for the data analysis. The selected sting balance had two moment gages that were mounted forward and aft of the balance moment center. The difference and the sum of the two gage outputs were fitted in the least squares sense using the normal force and the pitching moment at the balance moment center as independent variables. The regression model search algorithm predicted that the difference of the gage outputs should be modeled using the intercept and the normal force. The sum of the two gage outputs, on the other hand, should be modeled using the intercept, the pitching moment, and the square of the pitching moment. Equations of the deflection of a cantilever beam are used to show that the search algorithm s two recommended math models can also be obtained after performing a rigorous theoretical analysis of the deflection of the sting balance under load. The analysis of the sting balance calibration data set is a rare example of a situation when regression models of balance calibration data can directly be derived from first principles of physics and engineering. In addition, it is interesting to see that the search algorithm recommended the same regression models for the data analysis using only a set of statistical quality metrics.
Document ID
20090033643
Acquisition Source
Ames Research Center
Document Type
Extended Abstract
Authors
Ulbrich, Norbert
(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, 2009
Subject Category
Numerical Analysis
Report/Patent Number
ARC-E-DAA-TN259
Report Number: ARC-E-DAA-TN259
Meeting Information
Meeting: 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference
Location: Denver, CO
Country: United States
Start Date: August 2, 2009
End Date: August 5, 2009
Sponsors: American Society for Electrical Engineers, American Society of Mechanical Engineers, Society of Automotive Engineers, Inc., American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA04BA85C
Distribution Limits
Public
Copyright
Public Use Permitted.
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