Massive flow separation from the surface of a plane bluff obstacle in an incompressible uniform stream is addressed theoretically for large values of the global Reynolds number Re. The analysis is motivated by a conclusion drawn from recent theoretical results which is corroborated by experimental findings but apparently contrasts with common reasoning: the attached boundary layer extending from the front stagnation point to the position of separation never attains a fully developed turbulent state, even for arbitrarily large Re. Consequently, the boundary layer exhibits a certain level of turbulence intensity that is linked with the separation process, governed by local viscous-inviscid interaction. Eventually, the latter mechanism is expe...
A brief overview of flow separation phenomena is provided. Langley has many active research programs...
Researchers have understood the significance of boundary layers in the process of separation since \...
AbstractIncipient separation of shock/boundary-layer interactions (SBLIs) is reexamined through RANS...
An investigation was conducted on a turbulent boundary layer near a smooth surface with pressure gra...
Separating turbulent boundary layers occur in many practical engineering applications. Nonetheless, ...
May 1962Includes bibliographical referencesPreliminary reportThe phenomenon of incompressible bounda...
Massive turbulent separations are common phenomena that can cause sizeable aerodynamical losses and ...
We present large-eddy simulations (LES) of separation and reattachment of a flat-plate turbulent bou...
We present large-eddy simulations (LES) of separation and reattachment of a flat-plate turbulent bou...
Massive separation on airfoils operating at high Reynolds number is an important problem to the aero...
The exact transport equations for turbulent (Reynolds) stresses have left-hand sides representing th...
Numerical methods are used to investigate the separated flow over a finite flat plate when the flow ...
Numerical methods are used to investigate the separated flow over a finite flat plate when the flow ...
An experimental investigation of the effects of the geometry of body surface, Reynolds number, strea...
A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even wit...
A brief overview of flow separation phenomena is provided. Langley has many active research programs...
Researchers have understood the significance of boundary layers in the process of separation since \...
AbstractIncipient separation of shock/boundary-layer interactions (SBLIs) is reexamined through RANS...
An investigation was conducted on a turbulent boundary layer near a smooth surface with pressure gra...
Separating turbulent boundary layers occur in many practical engineering applications. Nonetheless, ...
May 1962Includes bibliographical referencesPreliminary reportThe phenomenon of incompressible bounda...
Massive turbulent separations are common phenomena that can cause sizeable aerodynamical losses and ...
We present large-eddy simulations (LES) of separation and reattachment of a flat-plate turbulent bou...
We present large-eddy simulations (LES) of separation and reattachment of a flat-plate turbulent bou...
Massive separation on airfoils operating at high Reynolds number is an important problem to the aero...
The exact transport equations for turbulent (Reynolds) stresses have left-hand sides representing th...
Numerical methods are used to investigate the separated flow over a finite flat plate when the flow ...
Numerical methods are used to investigate the separated flow over a finite flat plate when the flow ...
An experimental investigation of the effects of the geometry of body surface, Reynolds number, strea...
A mathematically simple, turbulence closure model designed to treat transonic airfoil flows even wit...
A brief overview of flow separation phenomena is provided. Langley has many active research programs...
Researchers have understood the significance of boundary layers in the process of separation since \...
AbstractIncipient separation of shock/boundary-layer interactions (SBLIs) is reexamined through RANS...