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Analysis Methods for Progressive Damage of Composite StructuresThis 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.
Document ID
20140001002
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Rose, Cheryl A.
(NASA Langley Research Center Hampton, VA, United States)
Davila, Carlos G.
(NASA Langley Research Center Hampton, VA, United States)
Leone, Frank A.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
March 4, 2014
Publication Date
July 1, 2013
Subject Category
Composite Materials
Report/Patent Number
NASA/TM-2013-218024
L-20257
NF1676L-16590
Funding Number(s)
WBS: WBS 794072.02.07.03.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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