© 2016, The Author(s).Pitching flat plates are a useful simplification of flapping wings, and their study can provide useful insights into unsteady force generation. Non-circulatory and circulatory lift producing mechanisms for low Reynolds number pitching flat plates are investigated. A series of experiments are designed to measure forces and study the unsteady flowfield development. Two pitch axis positions are investigated, namely a leading edge and a mid-chord pitch axis. A novel PIV approach using twin laser lightsheets is shown to be effective at acquiring full field of view velocity data when an opaque wing model is used. Leading-edge vortex (LEV) circulations are extracted from velocity field data, using a Lamb–Oseen vortex fitting ...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
An experimental study of two-dimensional pitching and plunging airfoils at low Reynolds number (Re) ...
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...
This paper analyses experimentally, the influence of the Leading EdgeVortex (LEV) on lift production...
We discuss implementation of prescribed-motion rigs, dye injection and direct force measurement for ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90618/1/AIAA-2011-872-285.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97118/1/AIAA2012-51.pd
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90678/1/AIAA-2011-3118-471.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90670/1/AIAA-2011-220-550.pd
The present study is a prelude to applying different flow control devices on pitching and plunging a...
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
This article describes a simple low-order model for the lift produced by rapidly accelerating and pi...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
An experimental study of two-dimensional pitching and plunging airfoils at low Reynolds number (Re) ...
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...
This paper analyses experimentally, the influence of the Leading EdgeVortex (LEV) on lift production...
We discuss implementation of prescribed-motion rigs, dye injection and direct force measurement for ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90618/1/AIAA-2011-872-285.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97118/1/AIAA2012-51.pd
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90678/1/AIAA-2011-3118-471.pd
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/90670/1/AIAA-2011-220-550.pd
The present study is a prelude to applying different flow control devices on pitching and plunging a...
This paper discusses the force history and flow topology of accelerating flat-plate wings. The work ...
This article describes a simple low-order model for the lift produced by rapidly accelerating and pi...
The simple canonical problem of a two-dimensional wing profile undergoing a single linear pitch-up/p...
An experimental study of two-dimensional pitching and plunging airfoils at low Reynolds number (Re) ...
The AIAA Fluid Dynamics Technical Committee\u27s Low Reynolds Number Discussion Group has introduced...