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Dynamic wind loads and wake characteristics of a wind turbine model in an atmospheric boundary layer wind
An experimental study was conducted to characterize the dynamic wind loads and evolution of the unsteady vortex and turbulent flow structures in the near wake of a horizontal axis wind turbine model
An Experimental Study of the Laminar Flow Separation on a Low-Reynolds-Number Airfoil
An experimental study was conducted to characterize the transient behavior of laminar flow separation on a NASA low-speed GA (W)-1 airfoil at the chord Reynolds number of 70,000. In addition to
An experimental study of a high-rise building model in tornado-like winds
Abstract An experimental study was conducted to quantify the characteristics of wake vortex and flow structures around a high-rise building model as well as the resultant wind loads (both forces and
An Experimental Investigation on Aerodynamic Hysteresis of a Low-Reynolds Number Airfoil
( ) An experimental study was conducted to investigate the aerodynamic characteristics of a NASA low speed GA(W)-1 airfoil at the chord Reynolds number of ReC=160,000. Aerodynamic hysteresis was
An experimental study of a bio-inspired corrugated airfoil for micro air vehicle applications
An experimental study was conducted to investigate the aerodynamic characteristics of a bio-inspired corrugated airfoil compared with a smooth-surfaced airfoil and a flat plate at the chord Reynolds
Characterization of the wind loads and flow fields around a gable-roof building model in tornado-like winds
An experimental study was conducted to quantify the characteristics of a tornado-like vortex and to reveal the dynamics of the flow-structure interactions between a low-rise, gable-roof building
Flexible-Membrane Airfoils at Low Reynolds Numbers
An experimental study was conducted to assess the benefits of using flexible-membrane airfoils/wings at low Reynolds numbers for micro air vehicle applications compared with using a conventional
Study of Trailing-Edge Cooling Using Pressure Sensitive Paint Technique
at five different blowing ratios between 0.4 and 1.6, both with and without moveable lands mounted on the trailingedge model. The measurement results indicate clearly that the blowing ratio and the
A study on a lobed jet mixing flow by using stereoscopic particle image velocimetry technique
In a continuing effort to study the mixing enhancement by large-scale streamwise vortices generated by a lobed nozzle, a high-resolution stereoscopic particle image velocimetry (PIV) system was used
Dual-plane stereoscopic particle image velocimetry: system set-up and its application on a lobed jet mixing flow
Abstract The technical basis and system set-up of a dual-plane stereoscopic particle image velocimetry (PIV) system, which can obtain the flow velocity (all three components) fields at two spatially
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