Page 96 - Template Tesis UTM v2.0
P. 96

that the peak stress and stiffness were higher in the in-plane direction. Moreover, it

                   was found that the peak stress and stiffness were highly dependent on the applied strain
                   rates, whereby the higher peak stress and stiffness were recorded at higher strain rates.

                   In addition, thicker laminate exhibited higher peak stress and stiffness in comparison
                   with thinner one.




                           Haque and Ali [121] investigated of S2-glass/vinyl ester on the compressive

                   properties and failure analysis using SHPB equipment. The comparison was also done
                   between dynamic and quasi-static properties of  compressive strength,  compressive

                   strain to failure and elastic modulus. During the quasi-static test, for unidirectional
                   laminate, loads were applied in fibre and transverse directions and only in fill direction

                   for plain-weave. The ultimate failure stress, failure strain and modulus were higher in
                   fibre direction with value of 201 MPa, 0.032 mm/mm and 6 GPa in comparison with

                   transverse direction of 80 MPa, 0.030 mm/mm and 2.5 GPa, respectively. For plain

                   weave S2-glass/vinyl ester, the ultimate failure stress, failure strain and modulus were
                   188 MPa, 0.036mm/mm, and 5 GPa respectively. When the applied load is parallel

                   with fibre direction, the dominant failures are the shear mode of microbuckling and
                   kink  band  formations  in  localized  areas.  These  kind  of  failure  modes  were  also

                   observed in plain weave laminates. However, when the load is in a transverse direction,
                   the failure started with matrix cracking which caused debonding and delamination.

                   However, it is interesting to note that fibre fracture did not occur at all, only resin

                   dominant failure modes. Both UD and plain weave specimens are strain rate dependent
                   with the higher failure strength and strain were recorded when the higher strain rates

                   applied.



                           Shaker et al. [108] used SHPB apparatus to investiagte the high strain rate

                   compression  properties  of  aramid  and  ultra-high  molecular  weight  polyethylene

                   (UHMWPE) composites in the out-of-plane direction at four different pressures of 2,4,
                   6 and 8 bar (to get the variation of strain rates). Both hybrid and non-hybrid specimens

                   exhibited the strain rate sensitivity. Initially, the stress showed a nearly linear increase
                   with  strain  and  become  non-linear  at  the  later  stage  of  deformation  with  further

                   increase  in  the  strain.  It  was  found  that  flow  stress  increased  with  the  increasing
                   pressure as can be seen when the stress-strain curves go up gradually. In addition, the



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