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.roneverhart.com/2006-LEXUS-GS300-Rear-Door-Paint-Code-1F2-Mercury-Metallic-Left-Driver-Side-LH/