This paper presents a framework of aeroelastic optimization design for high-aspect-ratio wing with large deformation. A highly flexible wing model for wind tunnel test is optimized subjected to multiple aeroelastic constraints. Static aeroelastic analysis is carried out for the beamlike wing model. using a geometrically nonlinear beam formulation coupled with the nonplanar vortex latt... https://www.darthomes.shop/product-category/totes/