Calibration 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...
Aerodynamic forces and moments on scaled models are measured in wind tunnels by multi-component stra...
Fundamental characteristics of design, calibration, and application of three-component moment balanc...
Occurrence of static divergence will result in a catastrophic failure of wind tunnel models supporte...
A new regression model search algorithm was developed that may be applied to both general multivaria...
A candidate math model search algorithm was developed at Ames Research Center that determines a reco...
A new approach is presented that uses a weighted least squares fit to analyze wind tunnel strain-gag...
A new global regression analysis method is discussed that predicts wind tunnel model weight correcti...
A non-iterative load prediction algorithm for strain-gage balances was developed for the NASA Ames U...
Sting-mounted models that undergo significant unsteady motion suffer from degraded data quality beca...
Two programs were developed to calculate the pitch and roll position of the conventional sting drive...
A new test was developed to assess the uniqueness of wind tunnel strain-gage balance load prediction...
The article describes the computational evaluation of the effect a belly mounted sting on the aerody...
Wind tunnel model support stings can be subjected to transient aerodynamic and inertial loads which ...
Two programs have been developed to calculate the pitch and roll angles of a wind-tunnel sting drive...
Aerodynamic forces and moments on scaled models are measured in wind tunnels by multi-component stra...
Aerodynamic forces and moments on scaled models are measured in wind tunnels by multi-component stra...
Fundamental characteristics of design, calibration, and application of three-component moment balanc...
Occurrence of static divergence will result in a catastrophic failure of wind tunnel models supporte...
A new regression model search algorithm was developed that may be applied to both general multivaria...
A candidate math model search algorithm was developed at Ames Research Center that determines a reco...
A new approach is presented that uses a weighted least squares fit to analyze wind tunnel strain-gag...
A new global regression analysis method is discussed that predicts wind tunnel model weight correcti...
A non-iterative load prediction algorithm for strain-gage balances was developed for the NASA Ames U...
Sting-mounted models that undergo significant unsteady motion suffer from degraded data quality beca...
Two programs were developed to calculate the pitch and roll position of the conventional sting drive...
A new test was developed to assess the uniqueness of wind tunnel strain-gage balance load prediction...
The article describes the computational evaluation of the effect a belly mounted sting on the aerody...
Wind tunnel model support stings can be subjected to transient aerodynamic and inertial loads which ...
Two programs have been developed to calculate the pitch and roll angles of a wind-tunnel sting drive...
Aerodynamic forces and moments on scaled models are measured in wind tunnels by multi-component stra...
Aerodynamic forces and moments on scaled models are measured in wind tunnels by multi-component stra...
Fundamental characteristics of design, calibration, and application of three-component moment balanc...
Occurrence of static divergence will result in a catastrophic failure of wind tunnel models supporte...