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Damage tolerance in filament-wound graphite/epoxy pressure vesselsGraphite/epoxy composites are extensively used in the aerospace and sporting goods industries due to their superior engineering properties compared to those of metals. However, graphite/epoxy is extremely susceptible to impact damage which can cause considerable and sometimes undetected reduction in strength. An inelastic impact model was developed to predict damage due to low-velocity impact. A transient dynamic finite element formulation was used in conjunction with the 3D Tsai-Wu failure criterion to determine and incorporate failure in the materials during impact. Material degradation can be adjusted from no degradation to partial degradation to full degradation. The developed software is based on an object-oriented implementation framework called Extensible Implementation Framework for Finite Elements (EIFFE).
Document ID
19950022948
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Simon, William E.
(Lamar Univ. Beaumont, TX, United States)
Ngueyen, Vinh D.
(Lamar Univ. Beaumont, TX, United States)
Chenna, Ravi K.
(Lamar Univ. Beaumont, TX, United States)
Date Acquired
September 6, 2013
Publication Date
July 1, 1995
Subject Category
Mechanical Engineering
Report/Patent Number
NASA-CR-198804
NAS 1.26:198804
Report Number: NASA-CR-198804
Report Number: NAS 1.26:198804
Accession Number
95N29369
Funding Number(s)
CONTRACT_GRANT: NAG9-698
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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