Structural and aerodynamic analyses of a hybrid trailing edge control surface of a fully morphing wing
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DOI: 10.1177/1045389x16641200
Abstract: In this article, the design and analysis of a hybrid trailing edge control surface of an unmanned aerial vehicle are presented. The structural design was performed to increase and decrease the camber of the control… read more here.
Keywords: control surface; hybrid trailing; trailing edge; control ... See more keywords