For wind tunnel measurements in closed-wall test sections, possible interference effects of the wind tunnel walls play an important role. Three-dimensional TAU simulations were performed for the transonic flow around an airfoil model in the adaptive-wall test section of the Transonic Wind Tunnel Göttingen (DNW-TWG) to investigate the existence of wind tunnel wall effects. The results revealed a global side wall interference that is affecting the entire flow around the model and a local side wall interference disturbing the flow in the supersonic regime
Reynolds averaged Navier–Stokes simulations of a static and pitching delta wing within three wind tu...
Numerical simulations of three dimensional flows in a prototype adaptive wall wind tunnel are conduc...
The boundary layers at the test section walls of a transonic wind tunnel are known to reduce the wal...
The wall interference effects present on three-dimensional models during wind tunnel testing are dif...
Various sources of error can cause discrepancies among flight test results, experimental measurement...
The experimental results from previous two-dimensional aerofoil measurements at the German Aerospace...
This report summarises a numerical investigation of a wing-tailplane interference configuration for ...
The DLR project iGREEN (Integrated Green Aircraft; 2007-2010) investigates the effects of increased ...
Parallel sidewalls are the standard bounding walls in wind tunnels when making a wind tunnel model f...
One of the inherent difficulties in utilizing a ventilated test section wind tunnel is the interacti...
It has been shown that the gap between an airfoil and the windtunnel wall can have a significant eff...
The 0.3m trisonic tunnel was modified recently to incorporate - a new model cart to enable the model...
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models...
An initial wind tunnel test was made to validate a new wall adaptation method for 3-D models in test...
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models...
Reynolds averaged Navier–Stokes simulations of a static and pitching delta wing within three wind tu...
Numerical simulations of three dimensional flows in a prototype adaptive wall wind tunnel are conduc...
The boundary layers at the test section walls of a transonic wind tunnel are known to reduce the wal...
The wall interference effects present on three-dimensional models during wind tunnel testing are dif...
Various sources of error can cause discrepancies among flight test results, experimental measurement...
The experimental results from previous two-dimensional aerofoil measurements at the German Aerospace...
This report summarises a numerical investigation of a wing-tailplane interference configuration for ...
The DLR project iGREEN (Integrated Green Aircraft; 2007-2010) investigates the effects of increased ...
Parallel sidewalls are the standard bounding walls in wind tunnels when making a wind tunnel model f...
One of the inherent difficulties in utilizing a ventilated test section wind tunnel is the interacti...
It has been shown that the gap between an airfoil and the windtunnel wall can have a significant eff...
The 0.3m trisonic tunnel was modified recently to incorporate - a new model cart to enable the model...
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models...
An initial wind tunnel test was made to validate a new wall adaptation method for 3-D models in test...
Computations using the DLR TAU code are presented to predict the effect of the wind tunnel on models...
Reynolds averaged Navier–Stokes simulations of a static and pitching delta wing within three wind tu...
Numerical simulations of three dimensional flows in a prototype adaptive wall wind tunnel are conduc...
The boundary layers at the test section walls of a transonic wind tunnel are known to reduce the wal...