NASA NTRS · 20140001002
Analysis Methods for Progressive Damage of Composite Structures
Abstract
This document provides an overview of recent accomplishments and lessons learned in the development of general progressive damage analysis methods for predicting the residual strength and life of composite structures. These developments are described within their State-of-the-Art (SoA) context and the associated technology barriers. The emphasis of the authors is on developing these analysis tools for application at the structural level. Hence, modeling of damage progression is undertaken at the mesoscale, where the plies of a laminate are represented as a homogenous orthotropic continuum. The aim of the present effort is establish the ranges of validity of available models, to identify technology barriers, and to establish the foundations of the future investigation efforts. Such are the necessary steps towards accurate and robust simulations that can replace some of the expensive and time-consuming "building block" tests that are currently required for the design and certification of aerospace structures.
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Rose, Cheryl A., Davila, Carlos G., Leone, Frank A.. 2013-07-01. Analysis Methods for Progressive Damage of Composite Structures. https://ntrs.nasa.gov/citations/20140001002
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