Soaring to New Heights: Investigating the Aeroelastic Stability of Composite Aircraft Wings

Combining the best aspects of helicopters and fixed-wing aircraft into a single vehicle has been a long-held ambition in the aerospace industry. From Leonardo da Vinci’s early drawings of an ‘aerial screw’ to the V-22 Osprey tiltrotor aircraft used by the U.S. military today, engineers have grappled with the challenge of creating aircraft capable of both vertical take-off and landing (VTOL) and high-speed forward flight. While helicopters offer unparalleled VTOL performance, their top speeds are limited to around 300 km/h. Fixed-wing aircraft offer greater speed but require long runways for take-off and landing. Reconciling these conflicting design requirements is a major challenge.