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A New Global Regression Analysis Method for the Prediction of Wind Tunnel Model Weight CorrectionsA new global regression analysis method is discussed that predicts wind tunnel model weight corrections for strain-gage balance loads during a wind tunnel test. The method determines corrections by combining "wind-on" model attitude measurements with least squares estimates of the model weight and center of gravity coordinates that are obtained from "wind-off" data points. The method treats the least squares fit of the model weight separate from the fit of the center of gravity coordinates. Therefore, it performs two fits of "wind- off" data points and uses the least squares estimator of the model weight as an input for the fit of the center of gravity coordinates. Explicit equations for the least squares estimators of the weight and center of gravity coordinates are derived that simplify the implementation of the method in the data system software of a wind tunnel. In addition, recommendations for sets of "wind-off" data points are made that take typical model support system constraints into account. Explicit equations of the confidence intervals on the model weight and center of gravity coordinates and two different error analyses of the model weight prediction are also discussed in the appendices of the paper.
Document ID
20140010278
Acquisition Source
Ames Research Center
Document Type
Conference Paper
Authors
Ulbrich, Norbert Manfred
(Jacobs Technology, Inc. Moffett Field, CA, United States)
Bridge, Thomas M.
(Jacobs Technology, Inc. Moffett Field, CA, United States)
Amaya, Max A.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
July 29, 2014
Publication Date
June 16, 2014
Subject Category
Research And Support Facilities (Air)
Ground Support Systems And Facilities (Space)
Report/Patent Number
ARC-E-DAA-TN14898
Report Number: ARC-E-DAA-TN14898
Meeting Information
Meeting: AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Location: Atlanta, Georgia
Country: United States
Start Date: June 16, 2014
End Date: June 20, 2014
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNA09DB39C
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
strain-gage balance
wind tunnel testing
model weight and center of gravity
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