• Normal vortex interaction with a loaded symmetrical blade 

  Doolan, C.J.; Coton, F.N.; Galbraith, R.A.McD. (1999)
• Active vibration control for the Kazan Ansat 

  Kindereit, B.; Bachmeyer, P.; Bondoux, A.; Swanson, D.; Bushuev, A. (2018)

  This paper presents a high-level overview of the implementation and the results of LORD�s OMNI Active Vibration Control System (AVCS) on Russian Helicopter�s Ansat helicopter platform as well as a brief description of ...
• Development of a civil light helicopter flight simulator for pilot training 

  Kazenmaier, U.; Gerboni, C.A.; Geluardi, S.; Olivari, M.; Richter, T.; Fichter, W.; Bülthoff, H.H. (2018)

  This paper aims at defining the necessary characteristics to develop a reliable and cheap helicopter flight simulator that could be used in flight schools for pilot training. The main contribution is the definition of ...
• Initial progress in developing a predictive simulation tool to inform helicopter ship operations 

  Memon, W.A.; White, M.D.; Owen, I. (2018)

  The study presented in this paper is part of the project underway at the University of Liverpool (UoL) to develop a high-fidelity simulation tool that has a predictive capability to inform and support Ship Helicopter ...
• Cabin safety sensitivity to the mechanical parameters of the main crashworthy stages 

  Astori, P.; Ramachandran, T. (2018)

  Crashworthy helicopters have energy absorbing concepts introduced into seats, subfloor and landing gears. These stages are always passive systems, usually triggered by a load level, and develop pre-set responses independently ...

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