Online Monitoring of Whirl Flutter during Wind Tunnel Testing
Flutter is a dynamic aeroelastic instability caused by interaction of unsteady aerodynamic forces with elastic vibration of the structure. At the so-called flutter critical velocity, the damping ratio of one system mode becomes zero. If the flow velocity is increased beyond this critical point, the damping ratio becomes negative and even smallest disturbances (e.g. turbulence) will lead to amplified oscillations and to mechanical failure of the airframe.