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.chiggate.com/igora-vibrance-4-99-medium-brown-violet-extra-sale/