To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimental investigation was carried out at the rotor test facility (RTG) of the German Aerospace Center (DLR) in Gottingen. In addition to former studies based on velocity fields from particle image velocimetry (PIV) in the current measurement also a background-oriented Schlieren (BOS) setup was used for the measurement of density gradients caused by the blade tip vortices. This gives the opportunity to combine velocity and density information to yield a highly detailed understanding of the vortex topology and development
A method for the reconstruction of 3D density distributions of blade tip vortices is presented. The ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
The tip vortex of a finite rotor blade tip model undergoing pitch oscillations is investigated by me...
To characterize the vortex system of a helicopter rotor with cyclic pitch, an experimental investiga...
An investigation on blade tip vortices of a sub-scale rotor under cyclic pitch conditions is carried...
The vortex system of four rotating and pitching DSA-9A blades was examined numerically and experimen...
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 this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
The aim of this work is the quantitative measurement of the positions and strengths of vortices. In ...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
The blade-tip vortex of a rotating and pitching DSA-9A blade was investigated numerically and experi...
The flow field around a helicopter is dominated by strong coherent vortices originating from the bla...
In this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
The background oriented Schlieren (BOS) technique was used to visualize the blade tip vortices of a ...
A method for the reconstruction of 3D density distributions of blade tip vortices is presented. The ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
The tip vortex of a finite rotor blade tip model undergoing pitch oscillations is investigated by me...
To characterize the vortex system of a helicopter rotor with cyclic pitch, an experimental investiga...
An investigation on blade tip vortices of a sub-scale rotor under cyclic pitch conditions is carried...
The vortex system of four rotating and pitching DSA-9A blades was examined numerically and experimen...
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 this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
The aim of this work is the quantitative measurement of the positions and strengths of vortices. In ...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
The blade-tip vortex of a rotating and pitching DSA-9A blade was investigated numerically and experi...
The flow field around a helicopter is dominated by strong coherent vortices originating from the bla...
In this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
The background oriented Schlieren (BOS) technique was used to visualize the blade tip vortices of a ...
A method for the reconstruction of 3D density distributions of blade tip vortices is presented. The ...
The advancement of measurement systems and technology keeps pushing experimental aerodynamics, which...
The tip vortex of a finite rotor blade tip model undergoing pitch oscillations is investigated by me...