Aeroelasticity is the study of how inertial, structural and aerodynamic forces interact on aircraft and structures. There are two main types: static and dynamic aeroelasticity. Static issues include divergence and control reversal, while dynamic issues include flutter and buffeting. The Boeing X-53 Active Aeroelastic Wing was a technology demonstrator aircraft that integrated wing aerodynamics, controls and structure to control wing twist at high speeds using leading edge flaps. This allowed the use of thin, high aspect ratio wings for improved high-speed rolling performance without adding stiffness for static aeroelastic issues.