Page 102 - Engineered Interfaces in Fiber Reinforced Composites
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Chapter  3.  Measurements  of  interfacelinterlaminar  properties   85

                stresses in the mid-plane, the crack propagation will be driven by the normal tensile
                stress to the laminar interface. At the onset of crack propagation, there may be an
                abrupt change in the stress-strain  curve (Fig 3.34(b)). The strain energy release rate,
                G,,  associated with edge delamination growth has been analyzed based on the rule
               of  mixtures  and  laminated  plate  theory,  assuming  the  absence  of  the  residual
               thermal  stresses. The constant  G, is derived  as a  function  of  the  critical  applied
                tensile strain, E~, and the laminate thickness 2h:
                   G, = t:h(E  - E’)  ,                                          (3.36)


               where  E’  is  the  effective Young’s  modulus  of  the  laminate  in  the  longitudinal
               direction during edge delamination. By  testing specimens made from laminates  of
               different stacking sequences, different percentages of mode I and mode I1 can also be
                obtained (O’Brien, 1984). Although the EDT specimen with starter cracks produces
                a mode I response, the data reduction scheme is complicated due to the presence of
               lamination  residual  stresses (see  Section 7.5.1). These  residual  stresses induce  an
               initial  outward  curvature  along  the  specimen edges, as schematically depicted  in
               Fig 3.34(c),  due  to  asymmetric  nature  of  the  specimen  above  and  below  the
               centerline. Such residual stresses can be very significant and the equation must be
               modified accordingly when residual stresses are included (Whitney,  1989).

               References

               Abdallah,  M.G. and Gascoigne, H.E. (1989). The influence of test fixture design on the Iosipescu shear
                  test for fiber composite materials. In  Test Methods for Design AIlowable for Fibrous Composites: 2nd
                  Vol. ASTM STP 1003, (C.C. Chamis ed.), ASTM, Philadelphia, PA, pp. 231-260.
               Adams,  D.F.  (1990).  The  Iosipescu  shear  test  method  as  used  for  testing  polymers  and  composite
                  materials. Polym. Composites  11, 286290.
               Adams,  D.F. and  Walrath,  D.E.  (1982). Iosipescu shear  properties  of  SMC composite  materials.  In
                  Composite  Materials:  Testing and Design  (Sixth Con$).  ASTM STP 787 (I.M. Daniel ed.), ASTM,
                  Philadelphia, PA, pp.  19-33.
               Adams, D.F. and Walrath, D.E. (1987a). Current status of the Iosipescu shear test method. J. Composite
                  Mater. 21, 49&507.
               Adams, D.F. and Walrath, D.E. (1987b). Further development of the Iosipescu shear test method. Exper.
                  Mech. 27, 113-1 19.
               Andersons, J. and Tamuzs, V. (1993). Fiber and interface strength distribution studies with the single fiber
                  composite test. Composites Sci. Technol. 48, 57-63.
               Asloun,  El. M., Nardin,  M. and Schultz, J. (1989). Stress transfer  in single-fiber composites: Effect of
                  adhesion, elastic modulus of fiber and matrix and polymer chain mobility. J. Mater. Sci. 24, 1835-1 844.
               ASTM D 2344 (1989). Test method for apparent interlaminar shear strength of parallel fiber composites
                  by  short-beam method.
               ASTM D 3039 (1982). Test method for tensile properties of fiber-resin  composites.
               ASTM  D  351 8  (1991). Practice  for  in-plane  shear  stress-strain  response  of  unidirectional  reinforced
                  plastics.
               ASTM D 3846 (1985).  Test method  for in-plane shear strength of reinforced plastics.
               ASTM D 4255 (1983). Guide for testing in plane shear properties of composite laminates.
               ASTM D 5528 (1994). Mode I interlaminar fracture toughness of unidirectional fiber-reinforced polymer
                  matrix composites.
               Baillie, C.A. (1991). Ph.D. Thesis, University of Surrey, Surrey, United  Kingdom.
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