MATEC Web of Conferences

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

Handrico Ramelan Pratama and Muhammad Agung Bramantya

MATEC Web Conf., 197 (2018) 08017

Published online: 12 September 2018

DOI: 10.1051/matecconf/201819708017

Handrico Ramelan Pratama

Muhammad Agung Bramantya

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