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NASA NTRS · 20040100698

A Damage-Dependent Finite Element Analysis for Fiber-Reinforced Composite Laminates

Abstract

A progressive damage methodology has been developed to predict damage growth and residual strength of fiber-reinforced composite structure with through penetrations such as a slit. The methodology consists of a damage-dependent constitutive relationship based on continuum damage mechanics. Damage is modeled using volume averaged strain-like quantities known as internal state variables and is represented in the equilibrium equations as damage induced force vectors instead of the usual degradation and modification of the global stiffness matrix.

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BibTeXRIS

Coats, Timothy W., Harris, Charles E.. 1998-01-01. A Damage-Dependent Finite Element Analysis for Fiber-Reinforced Composite Laminates. https://ntrs.nasa.gov/citations/20040100698

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