Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms
AbstractThis work focuses on the wake encounter problem occurring when a light, or very light, aircraft flies through or nearby a wind turbine wake. The dependency of the aircraft normal load factor on the distance from the turbine rotor in various flight and environmental conditions is quantified. For this research, a framework of software applications has been developed for generating and controlling a population of flight simulation scenarios in presence of assigned wind and turbulence fields. The JSBSim flight dynamics model makes use of several autopilot systems for simulating a realistic pilot behavior during navigation. The wind distribution, calculated with OpenFOAM, is a separate input for the dynamic model and is considered frozen during each flight simulation. The aircraft normal load factor during wake encounters is monitored at different distances from the rotor, aircraft speeds, rates of descent and crossing angles. Based on these figures, some preliminary guidelines and recommendations on safe encounter distances are provided for general aviation aircraft, with considerations on pilot comfort and flight safety. These are needed, for instance, when an accident risk assessment study is required for flight in proximity of aeolic parks. A link to the GitHub code repository is provided. View Full-Text
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Varriale, C.; De Marco, A.; Daniele, E.; Schmidt, J.; Stoevesandt, B. Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms. Aerospace 2018, 5, 42.
Varriale C, De Marco A, Daniele E, Schmidt J, Stoevesandt B. Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms. Aerospace. 2018; 5(2):42.Chicago/Turabian Style
Varriale, Carmine; De Marco, Agostino; Daniele, Elia; Schmidt, Jonas; Stoevesandt, Bernhard. 2018. "Flight Load Assessment for Light Aircraft Landing Trajectories in Windy Atmosphere and Near Wind Farms." Aerospace 5, no. 2: 42.
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