A pitch-up, hold, pitch-down motion for a flat plate is studied using theoretical, computational (immersed boundary method), and experimental (water-tunnel) methods. This motion is one of several canonical pitch motions introduced by the AIAA Fluid Dynamics Technical Committee's Low Reynolds Number Discussion Group. An inviscid theoretical method that is applicable to non-periodic motions and that accounts for large amplitudes and nonplanar wakes is employed. Results from theory are compared against those from computation and experiment which are also compared with each other. The variation of circulatory and apparent-mass loads as a function of pivot location for this motion is examined. The flow phenomena leading up to leading edge vortex...
Point vortex calculations are compared to experimental results for a 2D pitching and plunging airfoi...
This paper analyses experimentally, the influence of the Leading EdgeVortex (LEV) on lift production...
A numerical simulation of two and three-dimensional pitching and plunging flat plate at Reynolds num...
A pitch-up, hold, pitch-down motion for a flat plate is studied using theoretical, computational (im...
We discuss implementation of prescribed-motion rigs, dye injection and direct force measurement for ...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90618/1/AIAA-2011-872-285.pd
The AIAA Fluid Dynamics Technical Committee\u27s Low Reynolds Number Discussion Group has introduced...
© 2016, The Author(s).Pitching flat plates are a useful simplification of flapping wings, and their ...
The understanding of low Reynolds number aerodynamics is becoming increasingly prevalent with the re...
A combined numerical and experimental study of two- and three-dimensional pitching and plunging flat...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97118/1/AIAA2012-51.pd
In this paper we simulate the unsteady, incompressible, and laminar flow behavior over a flat plate ...
Using qualitative and quantitative flow visualization, we revisit the classical unsteady aerodynamic...
In the present study, we use numerical simulations to investigate the three-dimensional flows over l...
Point vortex calculations are compared to experimental results for a 2D pitching and plunging airfoi...
This paper analyses experimentally, the influence of the Leading EdgeVortex (LEV) on lift production...
A numerical simulation of two and three-dimensional pitching and plunging flat plate at Reynolds num...
A pitch-up, hold, pitch-down motion for a flat plate is studied using theoretical, computational (im...
We discuss implementation of prescribed-motion rigs, dye injection and direct force measurement for ...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90618/1/AIAA-2011-872-285.pd
The AIAA Fluid Dynamics Technical Committee\u27s Low Reynolds Number Discussion Group has introduced...
© 2016, The Author(s).Pitching flat plates are a useful simplification of flapping wings, and their ...
The understanding of low Reynolds number aerodynamics is becoming increasingly prevalent with the re...
A combined numerical and experimental study of two- and three-dimensional pitching and plunging flat...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97118/1/AIAA2012-51.pd
In this paper we simulate the unsteady, incompressible, and laminar flow behavior over a flat plate ...
Using qualitative and quantitative flow visualization, we revisit the classical unsteady aerodynamic...
In the present study, we use numerical simulations to investigate the three-dimensional flows over l...
Point vortex calculations are compared to experimental results for a 2D pitching and plunging airfoi...
This paper analyses experimentally, the influence of the Leading EdgeVortex (LEV) on lift production...
A numerical simulation of two and three-dimensional pitching and plunging flat plate at Reynolds num...