A series of fatigue tests has been conducted to clarify the fracture behavior depending on the stacking sequences of quasiisotropic
CFRP laminates. Strips of laminate with four different directions were cut out from the same CFRP plate to prepare the
specimens with the four stacking sequences. Prior to fatigue tests, the specimens were collided by a lateral load in order to
simulate the damage induced by the fallen tools. During the fatigue tests, the damage developed in the specimen was detected
by non-destructive techniques such a scanning acoustic microscope (SAM) and a replicating method. Stacking sequences exerted
an influence on fracture behavior of laminate specimens, i.e., the stacking position of the zero degree layers, in which fiber
direction was parallel to the loading axis, played an important role in the fatigue process. When the zero degree layers were
located at the specimen surface, no remarkable damage progress was observed from the surface. On the other hand, when the
zero degree layers were located in the middle of laminates, the damage in the surface layer was found in the fatigue process. Not
only the degradation of the equivalent elastic modulus was seen in all specimens, but also the degradation curve varied with the
stacking sequences.
抄録全体を表示