Three-dimensional flow past an elliptic cylinder with an aspect ratio of 0.5 near a moving bottom wall is investigated numerically for gap ratios of /=0.1,0.2,0.3, and 0.4 (where G denotes the gap between the cylinder bottom and the moving wall, and D is the major-axis length of the cylinder) with Reynolds numbers (Re) ranging from 100 to 200 (based on a constant inlet velocity and the major-axis length of the cylinder); the transition between two- and three-dimensional flow regimes is described in detail. For /=0.4, the flow is first two-dimensional with a Kármán vortex street followed by a two-layered wake, then it evolves into a three-dimensional flow regime with near-wake and far-wake elliptic instabilities of vortex pairs; for ≥180, th...
Abstract In the present paper, the spatio-temporal evolution of the vorticity field in t...
The initially generated pure mode A, as a transitional stage, is investigated in the three-dimension...
A spatially local stability analysis is reported for the cylinder wake at Reynolds numbers 190 and 2...
The three-dimensional transition of the wake flow behind a circular cylinder is studied in detail by...
In this work, the flow over an elliptic cylinder near a moving wall is investigated for Reynolds num...
The flow past a circular cylinder in the transitional regime at Re = 2000 has been thoroughly invest...
Flow over elliptic cylinders can be considered prototypical of flow over a range of bluff bodies sin...
[[abstract]]In this study, near-critical bifurcations of low Reynolds number (Re) flows past a pair ...
Results are presented for finite element simulation of three-dimensional unsteady flows past cylinde...
The spatial evolution of vortices and transition to three-dimensionality in the wake of a square cyl...
Vortex shedding from an inclined circular cylinder at low values of Reynolds number (Re) is investig...
International audienceThis paper presents the characteristics of the different stages in the evoluti...
In the present paper, the spatio-temporal evolution of the vorticity field in the second wake instab...
The present work investigates the combined effect of the angle of attack (AOA) (the angle between th...
International audienceThis paper presents the results of numerical stability analysis of the wake of...
Abstract In the present paper, the spatio-temporal evolution of the vorticity field in t...
The initially generated pure mode A, as a transitional stage, is investigated in the three-dimension...
A spatially local stability analysis is reported for the cylinder wake at Reynolds numbers 190 and 2...
The three-dimensional transition of the wake flow behind a circular cylinder is studied in detail by...
In this work, the flow over an elliptic cylinder near a moving wall is investigated for Reynolds num...
The flow past a circular cylinder in the transitional regime at Re = 2000 has been thoroughly invest...
Flow over elliptic cylinders can be considered prototypical of flow over a range of bluff bodies sin...
[[abstract]]In this study, near-critical bifurcations of low Reynolds number (Re) flows past a pair ...
Results are presented for finite element simulation of three-dimensional unsteady flows past cylinde...
The spatial evolution of vortices and transition to three-dimensionality in the wake of a square cyl...
Vortex shedding from an inclined circular cylinder at low values of Reynolds number (Re) is investig...
International audienceThis paper presents the characteristics of the different stages in the evoluti...
In the present paper, the spatio-temporal evolution of the vorticity field in the second wake instab...
The present work investigates the combined effect of the angle of attack (AOA) (the angle between th...
International audienceThis paper presents the results of numerical stability analysis of the wake of...
Abstract In the present paper, the spatio-temporal evolution of the vorticity field in t...
The initially generated pure mode A, as a transitional stage, is investigated in the three-dimension...
A spatially local stability analysis is reported for the cylinder wake at Reynolds numbers 190 and 2...