“Wings of the Future” The Project The Partners Contact us
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Implementation of a flight simulator for  the reference aircraft (Piaggio P180) (n.5 pages)
Specimens of hybrid composite active materials for Laboratory tests
Design of specific equipment for tests  on specimens of hybrid composite  active materials
Design and manufacturing of a small scale model of the Future-Wing (n.3 pages)
Measurement of Future Wing Unit displacements (n.2 pages)
Geometry and numerical model of a  piezo-controlled and a std 2D wing section (n.4 pages)
Comparison between a piezo-controlled  wing and a wing equipped with an aileron Structural model of the piezo-wing (n.3 pages)
Fluid dynamic grid of the piezo-wing (n.2 pages)
Structural model of the aileron of the  standard wing (3D analysis)
Fluid dynamic grid relevant to the aileron of the standard wing (n.2 pages)
Results of the Fluid Structure Interaction analysis: comparison between the piezo- wing and the aileron-wing
Model of the reference aircraft: structural  model and aerodynamic grid (n.2 pages)
Model of the aircraft with morphing wings:  structural model and aerodynamic grid (n.3 pages)
Laboratory tests
Typical results of laboratory tests on specimens of hybrid composite active  materials
AEROELASTIC ANALYSIS
FUTURE WING UNIT
MATERIALS CHARACTERIZATION
FLIGHT SIMULATOR
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