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Indentation test was done on the carbon/epoxy with different thickness and ply

                   orientation  to  form  the  contact  law  by  using  the  method  of  least  squares.  From
                   experimental test, it can be concluded that laminate thickness significantly influenced

                   the  deflection  of  the  tested  specimens.  Thicker  specimen  exhibited  less  deflection
                   instead of larger deflection was observed on the thinner specimens [94].




                           Zhu et al. [95] investigated the quasi-static indentation test of carbon/glass

                   reinforced  epoxy  at  different  loading  conditions  of  0°,  45°  and  90°.  Compression
                   strength and modulus at 0°, 45° and 90° were 301.92, 125.52, 269.46 MPa and 6.67,

                   2.97, 6.62 GPa, respectively. Tested specimens showed a brittle failure, particularly at
                   axial directions (0° and 90°). Initial elastic deformation was recorded on the stress-

                   strain curves followed by nonlinear performance until complete failure.



                           Hachemane  et  al.  [46]  experimentally  investiagted  the  jute/epoxy-cork

                   sandwich on indentation test to evaluate the influence of cork density on the damage
                   behaviour of sandwich composite. It was found that the cork density influenced the

                   damage force, maximum force and damage size. Two corks with different densities

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                   were used in this study, namely 310 and 160 kg/m . Results indicated that the sandwich
                   panel  with  heavy  agglomerated  of  higher  cork  density  exhibited  a  weaker  energy

                   dissipation capacity which was 3.29 % lower than lighter cork.







                   2.14  Impact Response of Fibre Reinforced Polymer Composites



                           Low velocity impact test was conducted on S2/SC-15 glass/epoxy composite

                   to compare the response of the tested specimen with quasi-static indentation. Peak
                   energy of 30.7 J which was obtained from quasi-static indentation was applied in the

                   impact test. Low velocity impact was done at velocity 3.41 m/s. The results showed

                   that  the  tested  specimen  exhibited  higher  initial  stiffness  and  energy  absorption
                   capacity in comparison with quasi static indentations’ specimens. Contrary, maximum

                   force and displacement values were exhibited slightly higher in comparison with quasi
                   static indentation test of identical specimen. Significant intralaminar fracture (vertical




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