The results are described of measurements of the mean and fluctuating forces acting on low aspect ratio triangular prisms placed vertically on a plane, having isosceles triangularcross-section with 60° or 90° apex angles and aspect ratios ranging from 1.0 to 3.0. The tests are carried out in a wind-tunnel by varying the wind direction, y, between 0° and 180°, at a Reynolds number Re ≈ 1.2 x 105. Furthermore, for the model with apex angle of 60° and aspect ratio 3.0, flow visualizations with tufts and hot-wire measurements are performed, which permit to characterize the wake morphology as a function of wind direction and to assess that an alternate vortex shedding always exists, with a frequency that is roughly inversely proportional to the ...
The flow field behind triangular wings (aspect ratfos.of 0.67 to J) alone and in coribfnationwith a ...
Blunt trailing edge airfoils offer structural and aerodynamic advantages in modern wind turbine and ...
Trailing vortex structure of low aspect ratio wings was studied in a water tunnel at Reynolds number...
The results are described of measurements of the mean and fluctuating forces acting on low aspect-ra...
The results are described of the measurement of the mean and fluctuating forces acting on triangular...
The velocity fluctuations experimentally detected in the wake of a prism ha- ving triangular cross-s...
Abstract. The results are described of experiments carried out to investigate on the connec-tion bet...
The results are described of experiments carried out to investigate on the connection between the fl...
The flow around two-dimensional or infinite square prisms has been extensively studied. Fewer publi...
Experiments are carried out to investigate on the connection between flow fluctuations and dynamics ...
Turbulent flow structure around a square prism of finite length is experimentally investigated in a ...
This research is aimed at depicting Reynolds number effect on bluff-body shapes with sharp edges. Ni...
The flow around a finite square prism has not been studied extensively when compared with an “infini...
Wind tunnel tests and large eddy simulations were conducted to investigate the dependency of wind fo...
Three-dimensional flow features of the slender rectangular prism with cross-section height (H) to st...
The flow field behind triangular wings (aspect ratfos.of 0.67 to J) alone and in coribfnationwith a ...
Blunt trailing edge airfoils offer structural and aerodynamic advantages in modern wind turbine and ...
Trailing vortex structure of low aspect ratio wings was studied in a water tunnel at Reynolds number...
The results are described of measurements of the mean and fluctuating forces acting on low aspect-ra...
The results are described of the measurement of the mean and fluctuating forces acting on triangular...
The velocity fluctuations experimentally detected in the wake of a prism ha- ving triangular cross-s...
Abstract. The results are described of experiments carried out to investigate on the connec-tion bet...
The results are described of experiments carried out to investigate on the connection between the fl...
The flow around two-dimensional or infinite square prisms has been extensively studied. Fewer publi...
Experiments are carried out to investigate on the connection between flow fluctuations and dynamics ...
Turbulent flow structure around a square prism of finite length is experimentally investigated in a ...
This research is aimed at depicting Reynolds number effect on bluff-body shapes with sharp edges. Ni...
The flow around a finite square prism has not been studied extensively when compared with an “infini...
Wind tunnel tests and large eddy simulations were conducted to investigate the dependency of wind fo...
Three-dimensional flow features of the slender rectangular prism with cross-section height (H) to st...
The flow field behind triangular wings (aspect ratfos.of 0.67 to J) alone and in coribfnationwith a ...
Blunt trailing edge airfoils offer structural and aerodynamic advantages in modern wind turbine and ...
Trailing vortex structure of low aspect ratio wings was studied in a water tunnel at Reynolds number...