Aircraft Structural Dynamics and Aeroelasticity Approaches: Recent Contributions from the Aerospace Engineering of Middle East Technical University, Türkiye

This study presents the details and also gives some preliminary results of current and ongoing research about the alleviation of aeroelastic instabilities of some air vehicles and helicopter structural dynamics. Studies about the characteristics of wrap around fins, generic new generation unmanned air vehicles and analyses considering the transonic aerodynamics of aircraft are presented. The article also attempts the aeroelastic analyses and structural dynamics of helicopters.