A morphing wing concept allowing for coupled twist-camber shape adaptation is proposed. The design is based on an optimized thickness distribution both spanwise and chordwise to be able to morph the wing sections into targeted airfoil shapes. Simultaneously. the spanwise twist is affected by the actuation. https://upffasonndods.aioblogs.com/87843449/observações-sobre-anofelinos-em-santa-catarina-brasil