Publication Date:
2019-07-13
Description:
A 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.
Keywords:
Research and Support Facilities (Air); Ground Support Systems and Facilities (Space)
Type:
ARC-E-DAA-TN14898
,
AIAA Aviation 2014; Jun 16, 2014 - Jun 20, 2014; Atlanta, Georgia; United States|AIAA Aerodynamic Measurement Technology and Ground Testing Conference; Jun 16, 2014 - Jun 20, 2014; Atlanta, Georgia; United States
Format:
application/pdf
Permalink