The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PIV technique experimentally in low Reynolds number, about 33 thousands. The mean velocity field is close to the 2D case, however the instantaneous structure is highly dynamical and 3D. Dynamics of the vortices in the boundary layer has been analysed using POD method. The results show lag of coherence in the streamwise direction, oblique patterns are detected instead
The global flow-field around an airfoil will be studied using time-resolved PIV technique. Interacti...
A combined approach of time resolved particle image velocimetry and a proper orthogonal decompositio...
The multi-plane stereo PIV (MSPIV) technique has been applied to an investigation of the spatial and...
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Stereocopic PIV measurements from an artificially tripped boundary layer flow along a flat plate wit...
Abstract Boundary layer velocity vectors over a 16 % elliptic airfoil at a Reynolds number of 3×105 ...
An investigation of the development of an artificially induced turbulent spot in a laminar boundary ...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
The motivation of the experiments is to study the flow dynamics and topology behind an airfoil. The ...
Stereoscopic PIV measurements from an artificially tripped boundary layer flow a long a flat plate w...
The global flow-field around an airfoil will be studied using time-resolved PIV technique. Interacti...
A combined approach of time resolved particle image velocimetry and a proper orthogonal decompositio...
The multi-plane stereo PIV (MSPIV) technique has been applied to an investigation of the spatial and...
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
The structure of boundary layer on an airfoil suction side was studied using stereo time resolved PI...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Experimental study of the structure of the boundary layer on the suction side of a plate is to be pr...
Stereocopic PIV measurements from an artificially tripped boundary layer flow along a flat plate wit...
Abstract Boundary layer velocity vectors over a 16 % elliptic airfoil at a Reynolds number of 3×105 ...
An investigation of the development of an artificially induced turbulent spot in a laminar boundary ...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
The motivation of the experiments is to study the flow dynamics and topology behind an airfoil. The ...
Stereoscopic PIV measurements from an artificially tripped boundary layer flow a long a flat plate w...
The global flow-field around an airfoil will be studied using time-resolved PIV technique. Interacti...
A combined approach of time resolved particle image velocimetry and a proper orthogonal decompositio...
The multi-plane stereo PIV (MSPIV) technique has been applied to an investigation of the spatial and...