Abstract:
Design of large space structures is restricted due to the limited storage capacity of
launch vehicles. Deployable structures made with ultra-thin woven fibre composites
eliminates this bottleneck due to self-deploying nature. These structures can selfdeploy
using
the
strain
energy
stored
during
elastic
folding. Popularity
of
selfdeployable
structures got
increased due to their
high
strength,
lightweight,
and
good
packaging
properties.
However,
thin woven
fibre composites
undergo
large
deformation
during
folding
process
due to the formation
of high
curvature,
which
causes
reduction
in bending
stiffness.
Hence,
it is crucial
to understand the mechanical
behaviour
of
these
structures
before
implementing,
in
order to avoid
unnecessary
failures.
Numerical
modelling
techniques
have
become
popular
in this research
area
due
to the advancement
of
computational methods
to obtain
the
mechanical
properties
of thin woven fibre composites. Homogenised Kirchhoff plate-based representative
unit cell modelling technique with solid elements is considered in this research.
Corresponding ABD stiffness matrices are obtained with using virtual work principle,
where the repetitive nature of woven fibre composites is represented by periodic
boundary conditions.
First, a series of micro-mechanical analyses is carried out to observe the influence of
the relative positioning of tows on the mechanical properties of thin woven fibre
composites. Various phase shifts between the plies have been considered in this
research which might be originated from the inter-ply misalignment during the
manufacturing stage. The outcomes of this parametric study clearly depict the variation
in in-plane and out-of-plane properties extracted from the ABD stiffness matrices and
describe the potential causes for the detected deviations between experimental and
numerical results.
Next, a resin embedded unit cell model is developed to predict the non-linear bending
behaviour with degree of deformation. Initially, a geometrically linear analysis is
carried out and then the analysis is extended to non-linear region to observe the
moment-curvature response. Linear analysis results of extensional stiffness and
Poisson’s ratio showed good agreement with the experimental results extracted from
the literature. However, the out-of-plane properties and shear stiffness values were
overpredicted. Similarly, non-linear analysis overpredicted the bending stiffness
throughout the considered curvature range. Hence, the resin embedded unit cell model
needs further improvements and modifications to accurately predict the out-of-plane
properties, and capture the reduction in bending stiffness.
Citation:
Gowrikanthan, N. (2023). Homogenized response of ultra-thin woven fibre composites under flexural loading [Master's theses, University of Moratuwa]. Institutional Repository University of Moratuwa. http://dl.lib.uom.lk/handle/123/22174