Nonlinear combined resonance of magneto-electro-elastic plates
European Journal of Mechanics - A/Solids,
Год журнала:
2024,
Номер
109, С. 105492 - 105492
Опубликована: Ноя. 8, 2024
Язык: Английский
Flat elliptical matrix crack impact on bending, stresses and stability of beam-like aerospace structures
Applied Mathematical Modelling,
Год журнала:
2025,
Номер
unknown, С. 115963 - 115963
Опубликована: Янв. 1, 2025
Язык: Английский
Nonlinear transient response analysis of revolution doubly curved shells
Archives of Civil and Mechanical Engineering,
Год журнала:
2025,
Номер
25(3)
Опубликована: Апрель 23, 2025
Язык: Английский
Nonlinear dynamics of the GPR porous cantilever twisted plate near veering regions
Y.X. Hao,
K. C. Sun,
H. Li
и другие.
Mechanics Based Design of Structures and Machines,
Год журнала:
2025,
Номер
unknown, С. 1 - 27
Опубликована: Март 20, 2025
Язык: Английский
Nonlinear internal resonances of rotating twisted multilayer functionally graded graphene nanoplatelet-reinforced composite blades
Yan Niu,
Renduo Song,
Yuejuan Yang
и другие.
Chaos Solitons & Fractals,
Год журнала:
2025,
Номер
195, С. 116340 - 116340
Опубликована: Март 25, 2025
Язык: Английский
Dynamic instability analysis of nature-inspired lattice microplates reinforced with graphene
Archive of Applied Mechanics,
Год журнала:
2025,
Номер
95(5)
Опубликована: Май 1, 2025
Язык: Английский
Resonant responses and double-parameter multi-pulse chaotic dynamics of FG-GP reinforced rotating pre-twisted composite laminated blade under combined transverse aerodynamic force and parametric excitations
Yuzhou Lian,
W. Zhang,
Y.F. Zhang
и другие.
Chaos Solitons & Fractals,
Год журнала:
2024,
Номер
189, С. 115725 - 115725
Опубликована: Ноя. 14, 2024
Язык: Английский
Nonlinear deflection and thermal post-buckling analysis of sector annular poroelastic composite nanodisks using mathematical simulation and machine learning algorithm
Thin-Walled Structures,
Год журнала:
2024,
Номер
207, С. 112702 - 112702
Опубликована: Ноя. 13, 2024
Язык: Английский
Snap-through of functionally graded graphene origami-enabled auxetic metamaterial doubly curved nonlinear shells
Mechanics Based Design of Structures and Machines,
Год журнала:
2024,
Номер
unknown, С. 1 - 20
Опубликована: Дек. 8, 2024
The
lightweight
design
of
thin-walled
curved
structures
as
spherical
shells
are
frequently
implemented
in
architecture,
aerospace,
mechanical,
automotive,
nuclear,
and
defense
structures.
Under
the
transverse
loads,
may
largely
deform
hence
snap
from
one
equilibrium
position
to
other.
Thus,
this
work
aims
develop
a
mathematical
model
computational
solution
investigate
nonlinear
bending
snap-through
behavior
doubly
auxetic
metamaterial
shell
subjected
transversal
loading,
for
first
time.
is
composed
several
layers
through
thickness,
each
layer
manufactured
copper
(Cu)
matrix
reinforced
with
specified
weight
fraction
graphene
origami
(GOAM).
mechanical
properties
GOAM
panel
presented
described
by
functions
volume
folding
degree.
Three
types
GOAM-distributions
considered,
which
U-type,
X-type,
O-type.
theoretical
framework
Kirchhoff–Love
hypotheses
thin
von
Karman
type
nonlinearity
used
derive
governing
equations.
differential
quadrature
method
(DQM)
discretize
space
domain
convert
partial
equation
algebraic
equations
terms
displacement
field.
An
efficient
incremental
iterative
procedure
developed
solve
predict
behavior.
A
conversion
validation
isotropic
considered.
Several
numerical
results
conducted
considering
effects
changing
content,
distribution
pattern,
degree,
curvature
thickness.
For
panels
exhibiting
behavior,
increasing
leads
higher
limiting
load;
however,
instability
gap
enlarged.
Язык: Английский
Numerical Study on the Static Bending Response of Cracked Wind Turbine Blades Reinforced with Graphene Platelets
Nanomaterials,
Год журнала:
2024,
Номер
14(24), С. 2020 - 2020
Опубликована: Дек. 16, 2024
With
the
growing
demand
for
wind
energy,
development
of
advanced
materials
turbine
support
structures
and
blades
has
garnered
significant
attention
in
both
industry
academia.
In
previous
research,
authors
investigated
incorporation
graphene
platelets
(GPLs)
into
blades,
focusing
on
structural
performance
cost-effectiveness
relative
to
conventional
fiberglass
composites.
These
studies
successfully
demonstrated
potential
advantages
GPL
reinforcement
improving
blade
reducing
blade’s
weight
costs.
Building
upon
prior
work,
present
study
conducts
a
detailed
investigation
static
bending
behavior
GPL-reinforced
specifically
examining
impact
crack
location
length.
A
finite
element
model
SNL
61.5
m
was
rigorously
developed
validated
through
comparison
with
existing
literature
ensure
its
accuracy.
Comprehensive
parametric
analyses
were
performed
assess
deflection
under
various
lengths
positions,
considering
flapwise
edgewise
deformations.
The
findings
indicate
that
exhibit
reduced
sensitivity
propagation
compared
traditional
blades.
Furthermore,
paper
presents
thorough
analysis
effects
length
performance.
Язык: Английский