“…Moreover, the proper balancing of the trailing edge could avoid flutter instability within the flight envelope. Rea et al [129] conducted an aeroelastic stability analysis of a wind-tunnel model equipped with a full-scale morphing aileron driven by load-bearing electromechanical actuators. The aim of their study was to prove that the concept is free from flutter up to 1.2 times the maximum expected flow speed (85m/s) during planned wind-tunnel tests.…”