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and  modulus  are  highly  dependent  on  the  strain  rate  whereby  higher  dynamic

                   compression properties were recorded by the tested specimens when the higher strain
                   rates were applied [116].




                           The  application  of  composite  materials  in  composite  armor  and  naval
                   structures required the characterisation of through thickness properties. Govender et

                   al.  [117] has conducted the quasi-static and SHPB tests on glass/vinyl ester specimens
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                   at 1.0 mm/min (   = 2.5 x 10-3 s ) and 5100 s , respectively. Result showed that the
                   higher the strain rate, the higher compressive strength is shown by the specimens. The

                   quasi-static exhibited the compressive stress of 417 MPa, which is 9.74 % less than
                   SHPB (462 MPa).




                           Song  et  al.  [118]  investigated  the  compressive  behaviour  of  woven

                   carbon/epoxy using SHPB apparatus. One-dimensional stress wave theory was applied
                   to determine the engineering stress, engineering strain and strain rate as shown in the

                   Equations 2.1, 2.2 and 2.3, respectively.




                                                 (  ) =                 (   +    +    )          (2.1)
                                                 
                                                                 
                                                                      
                                                                           
                                                        2     

                                                            
                                                (  ) =       ∫   (   +    +    )                 (2.2)
                                                                          
                                                                     
                                                                
                                                
                                                            0

                                                             
                                                  ̇ (  ) =  (   +    +    )                      (2.3)
                                                                         
                                                               
                                                   
                                                                    
                                                             

                   Meanwhile, wave speed can be determined using Equation 2.4 below;



                                                                    
                                                          = √                                    (2.4)
                                                          
                                                                    


                   Where;      and     are the cross-section area of the bars and specimen,    ,     and   
                                                                                                      
                                                                                               
                                                                                           
                               
                                      
                   are uniaxial elastic stress wave speed in pressure bars, density and Young’s modulus
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