Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76557/1/AIAA-30003-730.pd
The work presented in this paper undertakes a series of experiments to evaluate the basic structural...
A computational aeroelastic analysis of a micro air vehicle (MAV) is conducted. This MAV has a 24 in...
The characteristic feature of a mammalian flight is the use of thin compliant wings as the lifting ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76488/1/AIAA-2007-1067-747.pd
A low-aspect-ratio, low-Reynolds-number membrane wing has been identified as a viable platform for m...
A low aspect ratio, low Reynolds number membrane wing has been identified as a viable platform for m...
A low aspect ratio, low Reynolds number membrane wing has been identified as a viable platform for m...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76807/1/AIAA-2006-440-519.pd
The limited size of micro air vehicles (MAVs) requires small power sources, leading to a need for hi...
A modern class of Micro Aerial Vehicles (MAVs) uses Deformable Membrane Wings (DMWs), wing comprisin...
This work is concerned with wind tunnel testing of an elastic membrane wing intended for micro air v...
Micro air vehicles (MAVs) with a wingspan of 15 cm or shorter, and flight speed around 10 m/s have a...
The aerodynamic performance of a wing deteriorates considerably as the Reynolds number decreases fro...
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically challenging due to...
To lessen the deterioration of fixed-wing aerodynamic performance associated with chord Reynolds num...
The work presented in this paper undertakes a series of experiments to evaluate the basic structural...
A computational aeroelastic analysis of a micro air vehicle (MAV) is conducted. This MAV has a 24 in...
The characteristic feature of a mammalian flight is the use of thin compliant wings as the lifting ...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76488/1/AIAA-2007-1067-747.pd
A low-aspect-ratio, low-Reynolds-number membrane wing has been identified as a viable platform for m...
A low aspect ratio, low Reynolds number membrane wing has been identified as a viable platform for m...
A low aspect ratio, low Reynolds number membrane wing has been identified as a viable platform for m...
Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76807/1/AIAA-2006-440-519.pd
The limited size of micro air vehicles (MAVs) requires small power sources, leading to a need for hi...
A modern class of Micro Aerial Vehicles (MAVs) uses Deformable Membrane Wings (DMWs), wing comprisin...
This work is concerned with wind tunnel testing of an elastic membrane wing intended for micro air v...
Micro air vehicles (MAVs) with a wingspan of 15 cm or shorter, and flight speed around 10 m/s have a...
The aerodynamic performance of a wing deteriorates considerably as the Reynolds number decreases fro...
Fixed wing micro air vehicles (wingspan between 10 and 15 cm) are aerodynamically challenging due to...
To lessen the deterioration of fixed-wing aerodynamic performance associated with chord Reynolds num...
The work presented in this paper undertakes a series of experiments to evaluate the basic structural...
A computational aeroelastic analysis of a micro air vehicle (MAV) is conducted. This MAV has a 24 in...
The characteristic feature of a mammalian flight is the use of thin compliant wings as the lifting ...
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