Rotorcraft Aeromechanical Stability-Methodology Assessment. Phase 2. Workshop

摘要

Helicopter rotor aeroelastic and aeromechanical stability predictions for fourdata sets were made using industry and government stability analyses and compared with data at a workshop held at Ames Research Center, August 2-3, 1988. The present report contains the workshop comparisons. Keywords: Aeromechanic stability; Rotary wing aircraft; Aeroelastic stability; Rotorcraft dynamics; Aerodynamic stability; Aeroelasticity; Helicopter rotors. (edc)