Stereo PIV measurements has been performed behind the inclined plate, angle of attack 5 and 10 deg. Occurrence and dynamics of streamwise structures behind the plate trailing edge have been studied in details using POD method. The streamwise structures are represented by vortices and low- and highvelocity regions, probably streaks. The obtained results support the hypothesis of an airfoil-flow force interaction by Hoffman and Johnson [1,2]
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
The global flow-field around an airfoil will be studied using time-resolved PIV technique. Interacti...
The aim of this paper is to study the physics related to lift generation on an airfoil. A new hypoth...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
2D3C TR-PIV technique was utilized to investigate streamwise-oriented vortical structures behind an ...
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 experiments is to study the flow dynamics and topology behind an airfoil. The ...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
The wake behind an inclined plate simulating airfoil is to be studied experimentally. The vortical s...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to st...
A turbulent flow behind a simple thin planar air foil with rounded edges at moderate angle of attack...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
The global flow-field around an airfoil will be studied using time-resolved PIV technique. Interacti...
The aim of this paper is to study the physics related to lift generation on an airfoil. A new hypoth...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
2D3C TR-PIV technique was utilized to investigate streamwise-oriented vortical structures behind an ...
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 experiments is to study the flow dynamics and topology behind an airfoil. The ...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
The wake behind an inclined plate simulating airfoil is to be studied experimentally. The vortical s...
The presented study is focused on experimental investigation of a boundary layer on a flat plate in ...
The stereo PIV measurement were performed behind a wing in the plane perpendicular to the flow to st...
A turbulent flow behind a simple thin planar air foil with rounded edges at moderate angle of attack...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
The global flow-field around an airfoil will be studied using time-resolved PIV technique. Interacti...
The aim of this paper is to study the physics related to lift generation on an airfoil. A new hypoth...