Add to ORKGFlowfield measurements of the blade tip vortices from a rotating helicopter rotor model were performed by three component laser Doppler velocimetry (3D-LDV) and conventional (two component) particle image velocimetry (PIV). In general, the results are in good correspondence, but also illustrate the different properties of both techniques: LDV offers the capability of three-component measurements, whereas PIV captures the unsteadyness of the flowfiel
A first application of volumetric Particle Image Velocimetry (3D-PIV) was performed in 2005 with a H...
The advancement of flow measurement techniques continues to extend experimental boundaries and thus ...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
Flow field measurements of the blade tip vortices at a rotating helicopter rotor model were performe...
The measurement of three dimensional local flow vectors of a blade tip vortex at positions near the ...
With increasing use of civil helicopters the problem of noise emission of helicopters become more an...
The measurement of local flow vectors at positions near the helicopter rotor were performed with a t...
Particle image velocimetry (PIV) experiments have been performed in order to derive quantitative flo...
Particle image velocimetry (PIV) is increasingly used to investigate unsteady velocity fields instan...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
This work examined the wake aerodynamics of a single helicopter rotor blade with several tip shapes ...
Studies of the boundary layer profile and of the characteristics of the flow velocity distribution c...
3D Laser-Doppler-velocimeter measurements within the HART test campaign on a helicopter model rotor ...
The blade tip vortex of a full-scale MBB Bo 105 Helicopter is investigated experimentally under simu...
In order to investigate the development of blade tip vortices under different rotor conditions like ...
A first application of volumetric Particle Image Velocimetry (3D-PIV) was performed in 2005 with a H...
The advancement of flow measurement techniques continues to extend experimental boundaries and thus ...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
Flow field measurements of the blade tip vortices at a rotating helicopter rotor model were performe...
The measurement of three dimensional local flow vectors of a blade tip vortex at positions near the ...
With increasing use of civil helicopters the problem of noise emission of helicopters become more an...
The measurement of local flow vectors at positions near the helicopter rotor were performed with a t...
Particle image velocimetry (PIV) experiments have been performed in order to derive quantitative flo...
Particle image velocimetry (PIV) is increasingly used to investigate unsteady velocity fields instan...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
This work examined the wake aerodynamics of a single helicopter rotor blade with several tip shapes ...
Studies of the boundary layer profile and of the characteristics of the flow velocity distribution c...
3D Laser-Doppler-velocimeter measurements within the HART test campaign on a helicopter model rotor ...
The blade tip vortex of a full-scale MBB Bo 105 Helicopter is investigated experimentally under simu...
In order to investigate the development of blade tip vortices under different rotor conditions like ...
A first application of volumetric Particle Image Velocimetry (3D-PIV) was performed in 2005 with a H...
The advancement of flow measurement techniques continues to extend experimental boundaries and thus ...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...