Influence Of Contact Points of Skid Landing Gears on Helicopter Ground Resonance Stability

Soft-in-plane rotor systems are susceptible to a self-induced vibration phenomenon called ground resonance. This dynamic instability results from lag motions of the rotor blades coupling with airframe degrees of freedom while the helicopter is in ground contact. As an addition to previous slope landing studies and investigations of non-linear landing gear effects, this work focuses on a systematic study of partial skid contact using different landing modelling approaches and contact definitions. This paper is part of a larger study to investigate the influences of partial ground contact and soft terrain on helicopter dynamic stability during landings. It is the long-range objective to reduce the necessity of extensive flight tests prior to helicopter certification processes.