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A
a helicopter tail rotor
ABS
abstract
Active flutter control
active materials
active mounts
active structural acoustic control
active structure
Active Trailing-edge Flap blades
Actuated Fiber Composites
actuation systems
actuator
actuators
adaptive aeroelastic system
adaptive aircraft
Adaptive airfoil Wing
adaptive control
Adaptive Impact Absorption
Adaptronic Joint
Aerodynamic Load
aeroelastic instability
aeroservoelasticity
aerosol deposition method.
AFC
Airship
analog implementation
and Vibratory loads reduction analysis
are needed
as limit cycle oscillations
autonomous flap
B
Bend-twist coupling
Biomimetics
Biosensor
buckypaper
C
carbon black
Cell Mechanics.
charging dynamics
Clearance Adjustment
Compliant cellular structures
Compliant Mechanism
composite
composite thin walled beams
constitutive modeling
contractive
control.
controlled
Convection Coefficient
Cooling
corrugations
coupled modeling
Cross-coupling
D
ΔE effect
ΔE effect
ΔE(σ,H)
DEA
Deployable space structures
Dielectric elastomer
dielectric elastomer (DE)
distributed damping
E
EAP
electrical resistance
Electro active polymer (EAP)
Electro-active polymer
electroactive polymer
electroactive polymers
electromagnetic generator
Embedded Piezoelectric actuators
energy cycle
energy dissipation
energy harvesting
energy reduction
Environment
ESPI
F
failure
fast-sampling
FEA
FEM analysis
FGM
Fibre Bragg grating
finite element
Flexible skins
Flexure
fluid structure interaction
Flutter boundary prediction
frequency response
G
gain-scheduled control
Gurney Flap
H
H-Value
H8 controller design
Handling and assembly
helicopter tail rotor
Hierarchical modular systems
however
Humidity
I
ICAST 2008
identification
Impact
impact localisation
in the rotating frame
incompressible fluid
inflatable structure
inflatable structures
integral by parts
Integrated relative displacement sensor
intelligent materials
Intelligent tires
interlaminar shear
Iron-gallium alloys (Galfenol)
is generally difficult due
J
Jury's stability criterion
K
kinematics
L
Lamb wave
Lamb wave.
laminar wing
lco
Limit Cycle Oscillation
load control
M
macro-fiber composites
Magnetoelastic
Magnetorheological damper
Magnetostriction
mass reduction
measurement of these parameters
membrane actuator
Membrane elements
MEMS
MFC
mode shape
Mode-Tracking
modeling
modelling
Morphing
morphing aircraft
morphing airfoil
morphing structures
morphing wing
Motorcycle shock absorber
MR fluids
multi walled carbon nanotubes
Multi-stable composites
Multistable structures
MWCNT
N
Nanopositioning
Nanopositioning stage
Nitinol
Nonlinear Aeroelasticity
Nonlinear deformations.
nonlinear vibration
novel electronics
O
of dynamic instability such
Optimal design
optimization
optimization.
P
P3HT
packaging
parallel kinematics
Parallel Robot
parameter identification
Particle-stabilized foams
Passive Vibration Suppression
piezo actuator
piezoelectric
Piezoelectric Actuator
Piezoelectric buckling beam actuators
piezoelectric damping
Piezoelectric Elements
Piezoelectric Fibers.
piezoelectric generator
piezoelectric loudspeaker
piezoelectric materials
Piezoelectric Modal Constant
piezoelectric sensors
Piezoelectric transducer
Piezoelectricity
plastic yield
plate
Polyaniline
polymeric waveguide
position control
power factor
power harvesting
pressure sensor
pressurized structures
prosthetics
PVDF
PZT
R
Raster scanning.
remnant charges
remote sensing
Residual stress
robust control
Rotorcraft
S
sandwich
Scanning system
Self-sensing.
semi-active
semi-passive
Sensor
Shape
Shape Adaptation
Shape Control
Shape memory alloy
shape memory alloy (SMA)
shape memory alloys
shape memory effect
Shape memory polymers
shear stress transfer layer
shunt
simulation
skins
Sliding Mode
Slip Slope
SMA
Smart Fin
smart structure
smart structures
Space construction
space-charge electrets
speckle interferometry
Spiral folding
spool
spooling model.
SSHI
static aeroelasticity
Static and Dynamic Tests
strain actuation
Strain monitoring
stress waves
structural damping
structural design.
structural health monitoring
SU-8
subharmonic
switch
switching damping
Synthetic Jet Actuators
system design
system reliability
T
the aeroelastic parameters of
thermomechanical characterization
to evaluate the possibility
to the need to
Topology Optimization Method
tracking
transfer
Twist
U
unimorph actuator
V
Vapor
Variable camber airfoil
variable damping
variable geometry truss (VGT)
Variable Stiffness
vibration control
Vibration damping
vibration suppression
volume displacement
W
wire member actuators
Y
Young's modulus