Flow past an inclined flat plate at an angle of attack of 30° and a Reynolds number of 30 000 is investigated experimentally. The velocity field in the wake is measured with a laser doppler anemometer (LDA) in the region from one plate breadth downstream to three and a half-plate breadths downstream. Controlled forcing is applied to the wake by vibrating the plate in the across-wind direction at a frequency in the middle of the lock-in range. The forcing serves to enhance the regularity and two-dimensionality of vortex shedding from the plate. It also facilitates phase-locked averaging of the LDA data. The LDA bursts are sorted according to their arrival instants relative to a particular phase of the vortex shedding cycles. The phase-averag...
The near and very near wake of a thin flat plate with a circular trailing edge are investigated with...
Viscous flow around an oscillating vertical cylinder with a disk attached at keel is studied in deta...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...
This paper reports an experimental investigation of the vortex shedding wake behind a long flat plat...
The near wake of a flat plate is investigated via direct numerical simulations (DNS). Many earlier e...
The very near wake of a flat plate with a circular trailing edge, exhibiting pronounced shedding of ...
Vortex shedding flow from a flat plate inclined to a uniform flow at an angle of attack between 20° ...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...
A computational inquiry focuses on leading-edge vortex (LEV) growth and shedding during acceleration...
The near and very near wake of a flat plate with a circular trailing edge is investigated with data ...
Further experiments on features of the vortex shedding from tapered flat plates normal to an airstre...
Flow over an impulsively started low-aspect-ratio flat plate at angle-of-attack is investigated for ...
The present study is a prelude to applying different flow control devices on pitching and plunging a...
An experimental study of vortex shedding behind flat plates placed normal to an airstream is present...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
The near and very near wake of a thin flat plate with a circular trailing edge are investigated with...
Viscous flow around an oscillating vertical cylinder with a disk attached at keel is studied in deta...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...
This paper reports an experimental investigation of the vortex shedding wake behind a long flat plat...
The near wake of a flat plate is investigated via direct numerical simulations (DNS). Many earlier e...
The very near wake of a flat plate with a circular trailing edge, exhibiting pronounced shedding of ...
Vortex shedding flow from a flat plate inclined to a uniform flow at an angle of attack between 20° ...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...
A computational inquiry focuses on leading-edge vortex (LEV) growth and shedding during acceleration...
The near and very near wake of a flat plate with a circular trailing edge is investigated with data ...
Further experiments on features of the vortex shedding from tapered flat plates normal to an airstre...
Flow over an impulsively started low-aspect-ratio flat plate at angle-of-attack is investigated for ...
The present study is a prelude to applying different flow control devices on pitching and plunging a...
An experimental study of vortex shedding behind flat plates placed normal to an airstream is present...
NOTE: Text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in ...
The near and very near wake of a thin flat plate with a circular trailing edge are investigated with...
Viscous flow around an oscillating vertical cylinder with a disk attached at keel is studied in deta...
Open- and closed-loop control of vortex shedding in two-dimensional flow over a flat plate at high a...