SIte overview
Topic 1
Topic 2
Topic 3
Topic 4
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
s
pecimens
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
M
odel
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
s
pecimens
of
hybrid
composite
active
materials
AEROELASTIC ANALYSIS
FUTURE WING UNIT
MATERIALS CHARACTERIZATION
FLIGHT SIMULATOR
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