This paper reports an experimental investigation of the vortex shedding wake behind a long flat plate inclined at a small angle of attack to a main flow stream. Detailed velocity fields are obtained with particle-image velocimetry (PIV) at successive phases in a vortex shedding cycle at three angles of attack, α=20°, 25° and 30°, at a Reynolds number Re≈5,300. Coherent patterns and dynamics of the vortices in the wake are revealed by the phase-averaged PIV vectors and derived turbulent properties. A vortex street pattern comprising a train of leading edge vortices alternating with a train of trailing edge vortices is found in the wake. The trailing edge vortex is shed directly from the sharp trailing edge while there are evidences that the ...
Trailing edge and wake flows are of interest for a wide range of applications. Small changes in the ...
Further experiments on features of the vortex shedding from tapered flat plates normal to an airstre...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...
Flow past an inclined flat plate at an angle of attack of 30° and a Reynolds number of 30 000 is inv...
Vortex shedding flow from a flat plate inclined to a uniform flow at an angle of attack between 20° ...
The near wake of a flat plate is investigated via direct numerical simulations (DNS). Many earlier e...
This study focuses on the formation and detachment of a leading edge vortex (LEV) appearing on an ai...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
A computational inquiry focuses on leading-edge vortex (LEV) growth and shedding during acceleration...
This paper presents an experimental investigation of the vortex shedding in the wake of blunt and ob...
The present study is a prelude to applying different flow control devices on pitching and plunging a...
The flow-field behind an inclined plate was investigated experimentally using stereo PIV method prov...
The very near wake of a flat plate with a circular trailing edge, exhibiting pronounced shedding of ...
Viscous flow around an oscillating vertical cylinder with a disk attached at keel is studied in deta...
Flow over an impulsively started low-aspect-ratio flat plate at angle-of-attack is investigated for ...
Trailing edge and wake flows are of interest for a wide range of applications. Small changes in the ...
Further experiments on features of the vortex shedding from tapered flat plates normal to an airstre...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...
Flow past an inclined flat plate at an angle of attack of 30° and a Reynolds number of 30 000 is inv...
Vortex shedding flow from a flat plate inclined to a uniform flow at an angle of attack between 20° ...
The near wake of a flat plate is investigated via direct numerical simulations (DNS). Many earlier e...
This study focuses on the formation and detachment of a leading edge vortex (LEV) appearing on an ai...
The motivation of the presented study is supporting new ideas about principle of flight by Hoffman a...
A computational inquiry focuses on leading-edge vortex (LEV) growth and shedding during acceleration...
This paper presents an experimental investigation of the vortex shedding in the wake of blunt and ob...
The present study is a prelude to applying different flow control devices on pitching and plunging a...
The flow-field behind an inclined plate was investigated experimentally using stereo PIV method prov...
The very near wake of a flat plate with a circular trailing edge, exhibiting pronounced shedding of ...
Viscous flow around an oscillating vertical cylinder with a disk attached at keel is studied in deta...
Flow over an impulsively started low-aspect-ratio flat plate at angle-of-attack is investigated for ...
Trailing edge and wake flows are of interest for a wide range of applications. Small changes in the ...
Further experiments on features of the vortex shedding from tapered flat plates normal to an airstre...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...