The progress made at the development of modern flow measurement techniques such as Particle-Image Velocimetry (PIV) and Pressure Sensitive Paint (PSP) allow to provide flow data of increased quality and accuracy. Particularly PIV and PSP are able to capture a huge amount of experimental data during a wind tunnel test campaign. PIV provides instantaneous as well as averaged flow velocity fields in different planes of the flow and allows for the detection of large and small spatial flow structures. Using PSP the pressure distribution on a whole surface can be determined giving much more insight in details of the flow topology than would be possible by discrete pressure taps. The combined application of both techniques offers new possibilitie...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...
The pressure sensitive paint (PSP) and particle image velocimetry (PIV) techniques are applied to t...
The progress made at the development of modern flow measurement techniques as Particle-Image Velocim...
Visualization and measurements of aerodynamic effects on a delta-wing model and a 2D wing profile we...
For the International Vortex Flow Experiment 2 (VFE-2) new wind tunnel tests on a NASA delta-wing mo...
During the last decade several advanced non-intrusive image based measurement techniques such as pre...
Visualization of aerodynamic effects on a three-dimensional double-delta wing aircraft model was con...
The present paper describes the application of Particle Image Velocimetry (PIV) to the flow around a...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
In the past decades several image based measuring systems have been developed for industrial aerodyn...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile and a rotating delta-wing...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...
The pressure sensitive paint (PSP) and particle image velocimetry (PIV) techniques are applied to t...
The progress made at the development of modern flow measurement techniques as Particle-Image Velocim...
Visualization and measurements of aerodynamic effects on a delta-wing model and a 2D wing profile we...
For the International Vortex Flow Experiment 2 (VFE-2) new wind tunnel tests on a NASA delta-wing mo...
During the last decade several advanced non-intrusive image based measurement techniques such as pre...
Visualization of aerodynamic effects on a three-dimensional double-delta wing aircraft model was con...
The present paper describes the application of Particle Image Velocimetry (PIV) to the flow around a...
The pressure sensitive paint intensity and lifetime system (PSP) is an optical measurement technique...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
In the past decades several image based measuring systems have been developed for industrial aerodyn...
For investigations of pressure distributions on wind tunnel model surfaces with high spatial resolut...
Visualization and measurements of aerodynamic effects on a 2D-wing-profile and a rotating delta-wing...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
For investigations of flow fields with pronounced spatial structures and/or rapid temporal or spatia...
Visualization and measurements of aerodynamic effects on the three-dimensional aircraft model were c...