Results are presented for a wind tunnel experiment in which a screen element stretched spanwise across the floor of the test section is used. The screen element acts as a passive device introduced into the turbulent boundary layer in order to destroy its large-scale structure. Measurements are made for two streamwise locations of the screen element, for which the ratio of the screen height to the undisturbed boundary-layer thickness is 1.09 and 0.81, respectively. A marked increase in Clauser shape factor and decrease in skin friction are established. Relaxation characteristics as the perturbed boundary layer returns to equilibrium are discussed. The results point to the possibility of using the elimination of the large-scale coherent struc...
This paper examines the evolution of perturbations generated by various trips in a zero pressure gra...
A critical analysis of available compliant wall data which indicated drag reduction under turbulent ...
<p>Although various experimental studies have confirmed the potential drag reducing effect of dimple...
A passive device was introduced in a turbulent boundary layer to destroy its large scale structure. ...
Large scale motions in a turbulent boundary layer which is disturbed by a screen element are studied...
Recent experimental studies indicate that net drag reductions can be achieved in a turbulent boundar...
Experiments conducted since mid-seventies have shown that it is possible to insert bodies in turbule...
The effects of implementing a large-eddy break-up device (LEBU) in a turbulent boundary layer on the...
A computational study based on well-resolved large-eddy simulations is performed to study the skin f...
In this work, we experimentally investigate the effects of multiscale rough patches on the drag and ...
An experimental investigation at low airspeeds was made of the filling effect observed when a screen...
Initial measurements of the changes in local skin friction, velocity profile shape, and turbulence s...
Three devices that artificially increase the thickness of the boundary layer in a wind tunnel workin...
Subsonic wind tunnel experiments were conducted to study the effect of tripped boundary layer on the...
peer-reviewedThis work is devoted to the study of the influence of the freestream turbulence intensi...
This paper examines the evolution of perturbations generated by various trips in a zero pressure gra...
A critical analysis of available compliant wall data which indicated drag reduction under turbulent ...
<p>Although various experimental studies have confirmed the potential drag reducing effect of dimple...
A passive device was introduced in a turbulent boundary layer to destroy its large scale structure. ...
Large scale motions in a turbulent boundary layer which is disturbed by a screen element are studied...
Recent experimental studies indicate that net drag reductions can be achieved in a turbulent boundar...
Experiments conducted since mid-seventies have shown that it is possible to insert bodies in turbule...
The effects of implementing a large-eddy break-up device (LEBU) in a turbulent boundary layer on the...
A computational study based on well-resolved large-eddy simulations is performed to study the skin f...
In this work, we experimentally investigate the effects of multiscale rough patches on the drag and ...
An experimental investigation at low airspeeds was made of the filling effect observed when a screen...
Initial measurements of the changes in local skin friction, velocity profile shape, and turbulence s...
Three devices that artificially increase the thickness of the boundary layer in a wind tunnel workin...
Subsonic wind tunnel experiments were conducted to study the effect of tripped boundary layer on the...
peer-reviewedThis work is devoted to the study of the influence of the freestream turbulence intensi...
This paper examines the evolution of perturbations generated by various trips in a zero pressure gra...
A critical analysis of available compliant wall data which indicated drag reduction under turbulent ...
<p>Although various experimental studies have confirmed the potential drag reducing effect of dimple...