Abstract: This paper outlines the use of a three-dimensional topology optimization scheme for the conceptual design of compliant flapping micro air vehicle mechanisms. Each trilinear finite element within the design domain is assigned ...

Abstract: Micro air vehicles are typically characterized by a low aspect ratio wing operating at low Reynolds numbers

Abstract: The conceptual design of effective actuation mechanisms for flapping wing micro air vehicles presents considerable challenges, with competing weight, power, authority, and life cycle requirements. ...