Rotorcraft Flight Simulation Model Fidelity Improvement and Assessment

Rotorcraft flight dynamics simulation models require high levels of fidelity to be suitable as prime items in support of life cycle practices, particularly vehicle and control design and development, and system and trainer certification. On the civil side, both the FAA (US) and EASA (Europe) have documented criteria (metrics and practices) for...

Report to Novem, project no. 224.740-9854: Literature survey on aeromechanical instabilities for helicopters and wind turbines

Aeroelastic stability of modern windturbines: STABTOOL Final report phase 1

Report to Novem, project no. 224.740 9854: An investigation of the Rotor-Tower instability of the KEWT wind turbine

Report to Novem, project no. 224.740 9854: An investigation of the lead-lag instability of the Micon 1500/600 wind turbine