A first application of volumetric Particle Image Velocimetry (3D-PIV) was performed in 2005 with a HOver TIp vortex Structure test (HOTIS) in the rotor preparation hall of DLR Braun-schweig using a 40% Mach scaled model rotor of the Bo105. Major emphasis was placed on three component (3C) measurements in planes following each other as close as the resolution within each plane to form a 3D volume of the blade tip vortices. They were traced from their creation 1deg behind the trailing edge up to half a revolution. This paper deals with preliminary results obtained for vortex aging, RPM and thrust variation, and special effects observed in 3D volumetric data of young rotor blade tip vortices (age 3deg). In addition to PIV the background orient...
To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimen...
A method for the reconstruction of 3D density distributions of blade tip vortices is presented. The ...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade-...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
In order to investigate the development of blade tip vortices under different rotor conditions like ...
The blade tip vortex of a full-scale MBB Bo 105 Helicopter is investigated experimentally under simu...
Particle image velocimetry (PIV) experiments have been performed in order to derive quantitative flo...
Three-component (3-C) particle image velocimetry (PIV) measurements, within the wake across a rotor ...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
In the framework of the AIM project the near field of the blade tip vortex of a full-scale helicopte...
The measurement of local flow vectors at positions near the helicopter rotor were performed with a t...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade t...
Three-component (3-C) particle image velocimetry (PIV) measurements, within the wake across a rotor ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimen...
A method for the reconstruction of 3D density distributions of blade tip vortices is presented. The ...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade-...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
To investigate the development of blade tip vortices under different rotor conditions like thrust an...
In order to investigate the development of blade tip vortices under different rotor conditions like ...
The blade tip vortex of a full-scale MBB Bo 105 Helicopter is investigated experimentally under simu...
Particle image velocimetry (PIV) experiments have been performed in order to derive quantitative flo...
Three-component (3-C) particle image velocimetry (PIV) measurements, within the wake across a rotor ...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
In the framework of the AIM project the near field of the blade tip vortex of a full-scale helicopte...
The measurement of local flow vectors at positions near the helicopter rotor were performed with a t...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade t...
Three-component (3-C) particle image velocimetry (PIV) measurements, within the wake across a rotor ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimen...
A method for the reconstruction of 3D density distributions of blade tip vortices is presented. The ...
Noise and structural vibrations in rotorcraft are strongly influenced by interactions between blade-...