Mechanical properties of multidirectional fiber-reinforced composite laminates
are dispersive and random, and these uncertainties cause difficulties in safety
design of structures. So, it is necessary to analyze the sensitivity of
uncertain material properties on failure of structures. In this paper,
sensitivity analysis of uncertainties for composite laminates with different
stacking sequences and under various loadings is performed by the improved
Puck’s theory and the importance measurement analysis method. The improved
Puck’s theory with the in situ strength
effect which considers the influence of both the lamina itself and its
neighboring laminae can predict the initial and final failure accurately. Three
examples ([45°/0°/–45°/90°]2s laminates under uniaxial
tension, [0°/90°2/0°]s laminates
under uniaxial tension and biaxial tension) are examined, and results show that
the failure loads obey normal or log-normal distribution when the distribution
of uncertain material properties is log-normal. Results of sensitivity analysis
show that the longitudinal tensile strength of a unidirectional lamina has the
greatest influence on the final failure for laminated composites, and is
positive relative to final failure loads. As for initial failure, the influence
of each material property on failure is different because of different failure
mechanisms of composite laminates with different stacking sequences and under
various loadings. The results provide an in-depth understanding of the influence
of material properties on failure of composite laminates for safety
design.