We experimentally study the dynamics and strength of vortices shed from a NACA 0012 wing undergoing sinusoidal pitching in quiescent water. We characterize the temporal evolution of the vortex trajectory and circulation over a range of pitching frequencies, amplitudes and pivot locations. By employing a physics-based force and moment partitioning method (FMPM), we estimate the vortex-induced aerodynamic moment from the velocity fields measured using particle image velocimetry. The vortex circulation, formation time and vorticity-induced moment are shown to follow scaling laws based on the feeding shear-layer velocity. The vortex dynamics, together with the spatial distribution of the vorticity-induced moment, provide quantitative explanatio...
The motion of a two-dimensional buoyant vortex patch, i.e. a vortex patch with a uniform density dif...
Vortex formation and force generation of clapping plates with various aspect ratios (AR) and stroke...
Vortices are present in many fluid flows and depending on the context they may be either beneficial ...
Fluid flows interact with flexible and moving bodies in a wide range of natural and engineering appl...
This study focuses on the formation and detachment of a leading edge vortex (LEV) appearing on an ai...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90670/1/AIAA-2011-220-550.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90618/1/AIAA-2011-872-285.pd
This is the published version. Copyright © 2012 American Institute of PhysicsA two-dimensional nume...
In this study, an experimental investigation was performed to characterize the dynamic stall of pitc...
Wingtip vortices are generated by lifting airfoils; their salient features are compactness and relat...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...
A computational inquiry focuses on leading-edge vortex (LEV) growth and shedding during acceleration...
An investigation into redistribution of vorticity for rapidly accelerating plates with varying kinem...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
Small-scale aircraft, such as biological fliers and micro air vehicles, typically operate in a low R...
The motion of a two-dimensional buoyant vortex patch, i.e. a vortex patch with a uniform density dif...
Vortex formation and force generation of clapping plates with various aspect ratios (AR) and stroke...
Vortices are present in many fluid flows and depending on the context they may be either beneficial ...
Fluid flows interact with flexible and moving bodies in a wide range of natural and engineering appl...
This study focuses on the formation and detachment of a leading edge vortex (LEV) appearing on an ai...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90670/1/AIAA-2011-220-550.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90618/1/AIAA-2011-872-285.pd
This is the published version. Copyright © 2012 American Institute of PhysicsA two-dimensional nume...
In this study, an experimental investigation was performed to characterize the dynamic stall of pitc...
Wingtip vortices are generated by lifting airfoils; their salient features are compactness and relat...
The vortex produced at the leading edge of the wing, known as the leading edge vortex (LEV), plays a...
A computational inquiry focuses on leading-edge vortex (LEV) growth and shedding during acceleration...
An investigation into redistribution of vorticity for rapidly accelerating plates with varying kinem...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
Small-scale aircraft, such as biological fliers and micro air vehicles, typically operate in a low R...
The motion of a two-dimensional buoyant vortex patch, i.e. a vortex patch with a uniform density dif...
Vortex formation and force generation of clapping plates with various aspect ratios (AR) and stroke...
Vortices are present in many fluid flows and depending on the context they may be either beneficial ...