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Improvements to Constitutive Material Model for Fabrics

Abstract The high strength to weight ratio of woven fabric offers a cost effective solution to be used in a containment system for aircraft propulsion engines. Currently, Kevlar is the only Federal Aviation Administration (FAA) approved fabric for usage in systems intended to mitigate fan blade-out events. This research builds on an earlier constitutive model of Kevlar 49 fabric developed at Arizona State University (ASU) with the addition of new and improved modeling details. Latest stress strain experiments provided new and valuable data used to modify the material model post peak behavior. These changes reveal an overall improvement of the Finite Element (FE) model's ability to predict experimental results. First, the steel projectile is mode... (more)
Created Date 2011
Contributor Morea, Mihai Ion (Author) / Rajan, Subramaniam (Advisor) / Arizona State University (Publisher)
Subject Materials Science / Aerospace Engineering
Type Masters Thesis
Extent 120 pages
Language English
Reuse Permissions All Rights Reserved
Note M.S. Civil and Environmental Engineering 2011
Collaborating Institutions Graduate College / ASU Library
Additional Formats MODS / OAI Dublin Core / RIS

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Description Dissertation/Thesis