Evaluation of Novel Wing Design for UAV

P. K. Bahumanyam[1]
[1]University of Alabama in Huntsville, Huntsville, AL, USA
Veröffentlicht in 2014

Viable design alternative for the existing and fast growing UAVs which are optimized for unmanned flight is of great demand. Designing of a small scale UAV alternative to the AAI Aerosonde UAV has been considered changing the wing tail configuration of the vehicle analyzing both structural and aerodynamic performance improvements using COMSOL Multiphysics® software.