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wind tunnelSoftware
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models which are directly attached to the wind tunnel side-wall. Results show that the effect of the sidewalls is similar to an offset in the angle of attack (but can only partially be corrected by a change in alpha), and that this effect is proportional to the lift and Mach number. These results were used in the design phase for the iGREEN wing-tailplane interference experiment
To explore the influence of wind tunnel test facilities on delta wing aerodynamics, the interference...
It has been shown that the gap between an airfoil and the windtunnel wall can have a significant eff...
Tests have been made recent ly at ONERA on the interference effects arising from the presence of the...
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models...
The DLR project iGREEN (Integrated Green Aircraft; 2007-2010) investigates the effects of increased ...
This report summarises a numerical investigation of a wing-tailplane interference configuration for ...
The experimental results from previous two-dimensional aerofoil measurements at the German Aerospace...
For wind tunnel measurements in closed-wall test sections, possible interference effects of the wind...
Parallel sidewalls are the standard bounding walls in wind tunnels when making a wind tunnel model f...
Reynolds averaged Navier–Stokes simulations of a static and pitching delta wing within three wind tu...
The performance assessment of helicopter rotor blade airfoils no longer relies only on wind-tunnel t...
The performance assessment of helicopter rotor blade airfoils no longer relies only on wind-tunnel t...
For two reasons infinite-span swept wing flow is of interest: 1) the three-dimensional nature of th...
The IWEX wind tunnel model (Instationäres Wirbelexperiment, German for: Unsteady Vortex Experiment) ...
To explore the influence of wind tunnel test facilities on delta wing aerodynamics, the interference...
To explore the influence of wind tunnel test facilities on delta wing aerodynamics, the interference...
It has been shown that the gap between an airfoil and the windtunnel wall can have a significant eff...
Tests have been made recent ly at ONERA on the interference effects arising from the presence of the...
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models...
The DLR project iGREEN (Integrated Green Aircraft; 2007-2010) investigates the effects of increased ...
This report summarises a numerical investigation of a wing-tailplane interference configuration for ...
The experimental results from previous two-dimensional aerofoil measurements at the German Aerospace...
For wind tunnel measurements in closed-wall test sections, possible interference effects of the wind...
Parallel sidewalls are the standard bounding walls in wind tunnels when making a wind tunnel model f...
Reynolds averaged Navier–Stokes simulations of a static and pitching delta wing within three wind tu...
The performance assessment of helicopter rotor blade airfoils no longer relies only on wind-tunnel t...
The performance assessment of helicopter rotor blade airfoils no longer relies only on wind-tunnel t...
For two reasons infinite-span swept wing flow is of interest: 1) the three-dimensional nature of th...
The IWEX wind tunnel model (Instationäres Wirbelexperiment, German for: Unsteady Vortex Experiment) ...
To explore the influence of wind tunnel test facilities on delta wing aerodynamics, the interference...
To explore the influence of wind tunnel test facilities on delta wing aerodynamics, the interference...
It has been shown that the gap between an airfoil and the windtunnel wall can have a significant eff...
Tests have been made recent ly at ONERA on the interference effects arising from the presence of the...
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