Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76807/1/AIAA-2006-440-519.pd
To gain some more understanding of the flapping wing aerodynamics and aeroelasticity associated with...
Micro air vehicles (MAVs) with a wingspan of 15 cm or shorter, and flight speed around 10 m/s have a...
The static aeroelastic behavior of the Nighthawk mini unmanned aerial vehicle is examined using a co...
A class of micro air vehicles (MAVs), developed at the University of Florida, implements a flexible-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76488/1/AIAA-2007-1067-747.pd
A computational aeroelastic analysis of a micro air vehicle (MAV) is conducted. This MAV has a 24 in...
The Air Force Research Lab, Munitions Directorate, Eglin Air Force Base, Florida has designed a man-...
Experiments were systematically executed with a coupled computational fluid/structural dynamics aero...
This report describes research performed on various configurations of a flexible-wing Micro Air Vehi...
The limited size of micro air vehicles (MAVs) requires small power sources, leading to a need for hi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77149/1/AIAA-2008-615-169.pd
Due to their potential to expand our sensing and mission capabilities in both military and civilian ...
This work is concerned with wind tunnel testing of an elastic membrane wing intended for micro air v...
The work presented in this paper undertakes a series of experiments to evaluate the basic structural...
A modern class of Micro Aerial Vehicles (MAVs) uses Deformable Membrane Wings (DMWs), wing comprisin...
To gain some more understanding of the flapping wing aerodynamics and aeroelasticity associated with...
Micro air vehicles (MAVs) with a wingspan of 15 cm or shorter, and flight speed around 10 m/s have a...
The static aeroelastic behavior of the Nighthawk mini unmanned aerial vehicle is examined using a co...
A class of micro air vehicles (MAVs), developed at the University of Florida, implements a flexible-...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76488/1/AIAA-2007-1067-747.pd
A computational aeroelastic analysis of a micro air vehicle (MAV) is conducted. This MAV has a 24 in...
The Air Force Research Lab, Munitions Directorate, Eglin Air Force Base, Florida has designed a man-...
Experiments were systematically executed with a coupled computational fluid/structural dynamics aero...
This report describes research performed on various configurations of a flexible-wing Micro Air Vehi...
The limited size of micro air vehicles (MAVs) requires small power sources, leading to a need for hi...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77149/1/AIAA-2008-615-169.pd
Due to their potential to expand our sensing and mission capabilities in both military and civilian ...
This work is concerned with wind tunnel testing of an elastic membrane wing intended for micro air v...
The work presented in this paper undertakes a series of experiments to evaluate the basic structural...
A modern class of Micro Aerial Vehicles (MAVs) uses Deformable Membrane Wings (DMWs), wing comprisin...
To gain some more understanding of the flapping wing aerodynamics and aeroelasticity associated with...
Micro air vehicles (MAVs) with a wingspan of 15 cm or shorter, and flight speed around 10 m/s have a...
The static aeroelastic behavior of the Nighthawk mini unmanned aerial vehicle is examined using a co...
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