This paper compares the results of force and moment measurements made on the same test article and with the same balance in three transonic wind tunnels. Comparisons are made for the same combination of Reynolds number, Mach number, sideslip angle, control surface configuration, and angle of attack range. Between-tunnel force and moment differences are quantified. An analysis of variance was performed at four unique sites in the design space to assess the statistical significance of between-tunnel variation and any interaction with angle of attack. Tunnel to tunnel differences too large to attribute to random error were detected were observed for all forces and moments. In some cases these differences were independent of angle of attack and...
Abstract To measure the aerodynamic and hydrodynamic forces and moments acting on scaled models in w...
Two wind tunnel investigations were conducted to assess two different wall interference alleviation/...
The factors that determine data volume requirements in a typical wind tunnel test are identified. It...
This paper reports the result of an analysis of wind tunnel data acquired in support of the Facility...
The aerodynamic characteristics of two similar models of a lifting body configuration were run in tw...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
A new method is presented that computes a pre{test estimate of the upper bound of the drag coefficie...
Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the...
Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the...
A cooperative effort between the Office National d'Etudes et de Recherches Aerospatiales (ONERA); th...
Force and moment measurement capabilities are quintessential in wind tunnel testing. A force and mom...
Improvements and results of a new method are presented that computes a pre-test estimate of the prec...
Tests were conducted in the VKF/A and PWT/4T wind tunnels at AEDC to obtain captive trajectory, aero...
Aerodynamic analysis using computational fluid dynamics (CFD) is most fruitful when it is combined w...
Internal strain-gauge balances are multi-dimensional force transducers widely employed in wind tunne...
Abstract To measure the aerodynamic and hydrodynamic forces and moments acting on scaled models in w...
Two wind tunnel investigations were conducted to assess two different wall interference alleviation/...
The factors that determine data volume requirements in a typical wind tunnel test are identified. It...
This paper reports the result of an analysis of wind tunnel data acquired in support of the Facility...
The aerodynamic characteristics of two similar models of a lifting body configuration were run in tw...
In a series of wind tunnel tests, measurements were made of the aerodynamic loads acting on eight di...
A new method is presented that computes a pre{test estimate of the upper bound of the drag coefficie...
Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the...
Experimental aerodynamic investigations of the NASA Common Research Model have been conducted in the...
A cooperative effort between the Office National d'Etudes et de Recherches Aerospatiales (ONERA); th...
Force and moment measurement capabilities are quintessential in wind tunnel testing. A force and mom...
Improvements and results of a new method are presented that computes a pre-test estimate of the prec...
Tests were conducted in the VKF/A and PWT/4T wind tunnels at AEDC to obtain captive trajectory, aero...
Aerodynamic analysis using computational fluid dynamics (CFD) is most fruitful when it is combined w...
Internal strain-gauge balances are multi-dimensional force transducers widely employed in wind tunne...
Abstract To measure the aerodynamic and hydrodynamic forces and moments acting on scaled models in w...
Two wind tunnel investigations were conducted to assess two different wall interference alleviation/...
The factors that determine data volume requirements in a typical wind tunnel test are identified. It...