The Reynolds number and flaperon deflection influence taken into account when optimizing the wing airfoil of an unmanned aerial vehicle
Published: 19.11.2020
Authors: Kochurova N.I., Parkhaev Ye.S., Semenchikov N.V.
Published in issue: #11(107)/2020
DOI: 10.18698/2308-6033-2020-11-2030
Category: Aviation and Rocket-Space Engineering | Chapter: Aerodynamics and Heat Transfer Processes in Aircrafts