Numerical studies influence configuration fairing flap track airfoil type naca 4412 and naca 6412 character unmanned aerial vehicle (UAV)

Publisher: Edp Sciences

E-ISSN: 2261-236x|197|issue|08017-08017

ISSN: 2261-236x

Source: MATEC Web of conference, Vol.197, Iss.issue, 2018-09, pp. : 08017-08017

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Abstract