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High-Fidelity Aeroelastic Prediction

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Description

In the project "High-fidelity Aeroelastic Prediction" - funded by the Swiss Commission for Technology and Innovation (CTI) and Pilatus Aircraft Ltd - we focus on numerical aeroelasticity, i.e. on an approach based on the high-fidelity aerodynamic and structural description of an aircraft, aimed at predicting the dynamic behaviour of the latter throughout the flight envelope (altitude, mass and speed or Mach number).