NASA NTRS · 19930068777
A mechanics framework for a progressive failure methodology for laminated composites
Abstract
A laminate strength and life prediction methodology has been postulated for laminated composites which accounts for the progressive development of microstructural damage to structural failure. A damage dependent constitutive model predicts the stress redistribution in an average sense that accompanies damage development in laminates. Each mode of microstructural damage is represented by a second-order tensor valued internal state variable which is a strain like quantity. The mechanics framework together with the global-local strategy for predicting laminate strength and life is presented in the paper. The kinematic effects of damage are represented by effective engineering moduli in the global analysis and the results of the global analysis provide the boundary conditions for the local ply level stress analysis. Damage evolution laws are based on experimental results.
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Harris, Charles E., Allen, David H., Lo, David C.. 1989-10-01. A mechanics framework for a progressive failure methodology for laminated composites. https://ntrs.nasa.gov/citations/19930068777
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