Add to ORKGThe near wake of a flat plate with circular and elliptic trailing edges is investigated with data from direct numerical simulations. The plate length and thickness are the same in both cases. The separating boundary layers are turbulent and statistically identical. Therefore the wake is symmetric in the two cases. The emphasis in this study is on a comparison of the wake-distributions of velocity components, normal intensity and fluctuating shear stress obtained in the two cases
An experimental study of the developing two-dimensional turbulent wake behind a streamlined flat-pla...
Prepared under Bureau of Ships Fundamental Hydromechanics Research Program, Project S-R009 01 01 Con...
Three dimensional incompressible wake behind blunt obstacle located at leading edge of flat plat
The intermediate wake region of a thick flat plate with a circular trailing edge (TE) is investigate...
The near and very near wake of a flat plate with a circular trailing edge is investigated with data ...
The near wake of a flat plate is investigated via direct numerical simulations (DNS). Many earlier e...
The intermediate wakes of thin flat plates with circular trailing edges (TEs) are investigated here ...
The near and very near wake of a thin flat plate with a circular trailing edge are investigated with...
The near and very near wake of a flat plate with a circular trailing edge is investigated with data ...
The very near wake of a flat plate with a circular trailing edge, exhibiting pronounced shedding of ...
An experimental study has been conducted to investigate the far-field, self-similar properties of a ...
This paper investigates the characteristics of the turbulent wake structure developing from the trai...
Work is devoted to study of free-stream vorticity normal to leading edge interaction with boundary l...
Detailed measurements of two-dimensional profiles of static pressure, mean velocity, turbulence inte...
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
An experimental study of the developing two-dimensional turbulent wake behind a streamlined flat-pla...
Prepared under Bureau of Ships Fundamental Hydromechanics Research Program, Project S-R009 01 01 Con...
Three dimensional incompressible wake behind blunt obstacle located at leading edge of flat plat
The intermediate wake region of a thick flat plate with a circular trailing edge (TE) is investigate...
The near and very near wake of a flat plate with a circular trailing edge is investigated with data ...
The near wake of a flat plate is investigated via direct numerical simulations (DNS). Many earlier e...
The intermediate wakes of thin flat plates with circular trailing edges (TEs) are investigated here ...
The near and very near wake of a thin flat plate with a circular trailing edge are investigated with...
The near and very near wake of a flat plate with a circular trailing edge is investigated with data ...
The very near wake of a flat plate with a circular trailing edge, exhibiting pronounced shedding of ...
An experimental study has been conducted to investigate the far-field, self-similar properties of a ...
This paper investigates the characteristics of the turbulent wake structure developing from the trai...
Work is devoted to study of free-stream vorticity normal to leading edge interaction with boundary l...
Detailed measurements of two-dimensional profiles of static pressure, mean velocity, turbulence inte...
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
An experimental study of the developing two-dimensional turbulent wake behind a streamlined flat-pla...
Prepared under Bureau of Ships Fundamental Hydromechanics Research Program, Project S-R009 01 01 Con...
Three dimensional incompressible wake behind blunt obstacle located at leading edge of flat plat