The flow-field behind an inclined plate was investigated experimentally using stereo PIV method providing all 3 velocity vector components in the measuring plane. Flow structure in several measuring planes perpendicular to the main flow was studied. Statistical characteristics were evaluated in the measuring planes. The downwash angle was assessed as well to consider its effect on the lift generation mechanism. The dynamical behavior was studied using Proper Orthogonal Decomposition of velocity fields in measuring planes. The dominant (most energetic) structures were evaluated and presented. The detected structures are of the form of streamwise vortices combined with high-and low-velocity streaks
Stereocopic PIV measurements from an artificially tripped boundary layer flow along a flat plate wit...
This paper describes the investigation of the propeller slipstream at two different sideslip an-gles...
Flow past an inclined flat plate at an angle of attack of 30° and a Reynolds number of 30 000 is inv...
The flow-field behind an inclined plate was investigated experimentally using stereo PIV method prov...
The flow-field behind an inclined plate was investigated experimentally using stereo PIV method prov...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to st...
Stereo PIV measurements has been performed behind the inclined plate, angle of attack 5 and 10 deg. ...
2D3C TR-PIV technique was utilized to investigate streamwise-oriented vortical structures behind an ...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
This paper reports an experimental investigation of the vortex shedding wake behind a long flat plat...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
This thesis uses numerical investigations to examine details of the turbulent flow past bluff bodies...
The motivation of the experiments is to study the flow dynamics and topology behind an airfoil. The ...
The wake behind an inclined plate simulating airfoil is to be studied experimentally. The vortical s...
Stereocopic PIV measurements from an artificially tripped boundary layer flow along a flat plate wit...
This paper describes the investigation of the propeller slipstream at two different sideslip an-gles...
Flow past an inclined flat plate at an angle of attack of 30° and a Reynolds number of 30 000 is inv...
The flow-field behind an inclined plate was investigated experimentally using stereo PIV method prov...
The flow-field behind an inclined plate was investigated experimentally using stereo PIV method prov...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to st...
Stereo PIV measurements has been performed behind the inclined plate, angle of attack 5 and 10 deg. ...
2D3C TR-PIV technique was utilized to investigate streamwise-oriented vortical structures behind an ...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
This paper reports an experimental investigation of the vortex shedding wake behind a long flat plat...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
This thesis uses numerical investigations to examine details of the turbulent flow past bluff bodies...
The motivation of the experiments is to study the flow dynamics and topology behind an airfoil. The ...
The wake behind an inclined plate simulating airfoil is to be studied experimentally. The vortical s...
Stereocopic PIV measurements from an artificially tripped boundary layer flow along a flat plate wit...
This paper describes the investigation of the propeller slipstream at two different sideslip an-gles...
Flow past an inclined flat plate at an angle of attack of 30° and a Reynolds number of 30 000 is inv...