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But fatigue and fracture behavior of the laminates clearly deteriorates in corrosive conditions, although the results in case II are better than those in case I.
The analysis results were compared to the test results and investigated focusing on the geometrical nonlinearity and the micro-structural behavior of the laminates.
Under the defined load conditions, the homogenized stress-strain behavior of the laminates is obtained and then, the constitutive model parameters of the ply damage mesomodel are identified.
It is also deducted that if the ratio of layer thickness to plastic zone size is smaller than or equal to 1, the impact behavior of the laminates is sensitive to the interface strength.
Thermal fatigue tests were conducted on high temperature resistant carbon fiber reinforced plastics cross-ply laminates to evaluate microscopic damage progress which affects macroscopic mechanical behavior of the laminates.
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Behavior of the laminate is analyzed based on the first-order shear deformation theory.
Residual stress due to CTE thermal expansion mismatch is measured and the contribution of thermal residual stress to the failure behavior of the laminate is explored.
Numerical examples are considered and discussed to show the efficiency of the present semi-analytical solution and the effects of relevant parameters on the behavior of the laminate.
Additional mathematical difficulty is involved due to the presence of viscous interfaces because the behavior of the laminate depends on time.
Detailed discussion about how the absorbed moisture influenced the impact behavior of the laminate was carried out based on the interpretation of the damage characteristics and impact testing data.
Also, (B_{2} x,B_{66} xz,;{text{and}};, - frac{1}{2}B_{6} x^{2}) denote global terms that signify the general behavior of the laminate and V k (y) and W k (y) (k = 1, 2, …, N + 1) represent the local displacement components of all points located on the kth surface in the undeformed state (Reddy 2003; Nosier et al. 1993).
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