Add to ORKGThis paper concerns an investigation of a wing tip vortex of a modern transport aircraft in the transonic wind tunnel in Göttingen by means of the stereoscopic PIV and BOS method. Additionally to the velocity field perpendicular to the vortex line ca. 1/3 span behind the wing tip, the position and the density distribution of the vortex was determined in this area. The investigation of the density distribution was possible due to recent developments of the BOS postproccessing algorithms
Applications of an advanced schlieren technique, in the following referred to as Backround Oriented ...
In this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimen...
In case of Background Oriented Schlieren Method (BOS) and Particle Image Velocimetry (PIV) the infor...
The aim of this work is the quantitative measurement of the positions and strengths of vortices. In ...
Background-oriented schlieren (BOS) methods suited for large-scale and in-flight testing are present...
The background oriented Schlieren (BOS) technique was used to visualize the blade tip vortices of a ...
During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was inv...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
The background oriented Schlieren (BOS) method has been used to qualitatively identify the density g...
During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was inv...
In this paper we present the application of a novel schlieren technique for two different helicopter...
Wake vortex turbulence induced by large transport aircraft is problematic for airports’ capacity bec...
The Background Oriented Schlieren (BOS) method has been used to qualitatively identify the (variatio...
Vortex wakes of conventional aircraft and their propagating nature close to the ground have a great ...
Applications of an advanced schlieren technique, in the following referred to as Backround Oriented ...
In this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimen...
In case of Background Oriented Schlieren Method (BOS) and Particle Image Velocimetry (PIV) the infor...
The aim of this work is the quantitative measurement of the positions and strengths of vortices. In ...
Background-oriented schlieren (BOS) methods suited for large-scale and in-flight testing are present...
The background oriented Schlieren (BOS) technique was used to visualize the blade tip vortices of a ...
During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was inv...
A research topic of the Institute of Aerodynamics and Flow Technology in Göttingen is the investigat...
The background oriented Schlieren (BOS) method has been used to qualitatively identify the density g...
During a measurement with a MMB Bo 105 in Braunschweig, the rotor blade tip vortex position was inv...
In this paper we present the application of a novel schlieren technique for two different helicopter...
Wake vortex turbulence induced by large transport aircraft is problematic for airports’ capacity bec...
The Background Oriented Schlieren (BOS) method has been used to qualitatively identify the (variatio...
Vortex wakes of conventional aircraft and their propagating nature close to the ground have a great ...
Applications of an advanced schlieren technique, in the following referred to as Backround Oriented ...
In this paper, flow visualization of the blade vortices of four-bladed Mach-scaled rotor, as used in...
To characterize the vortex system of a rotor with collective and cyclic pitch settings, an experimen...