Aviation technologies, Vol 1, No 1 (2013)

UAV Wing Airfoil Aerodinamic Analyses

Aleksandr Lapušinskij (Lithuania)


The wing airfoils of an experimental UAV which is being designed at Antanas Gustaitis Aviation Institute is analysed and discussed. The wing airfoil characteristics when airfoil relative camber changes are being addressed. As a result, the most optimal wing airfoil used for targeted flight velocity interval is chosen.

Article in: Lithuanian

Article published: 2013-01-23

Keyword(s): UAV; airplane; aerodynamic; wing; airfoil

Full Text: PDF pdf


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