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Failure Strength of Nonlinearly Elastic Composite Laminates Containing a Pin Loaded Hole
dc.contributor.authorChang, Fu-Kuoen_US
dc.contributor.authorScott, Richarden_US
dc.contributor.authorSpringer, George S.en_US
dc.date.accessioned2010-04-13T19:53:39Z
dc.date.available2010-04-13T19:53:39Z
dc.date.issued1984en_US
dc.identifier.citationChang, Fu-Kuo; Scott, Richard; Springer, George (1984). "Failure Strength of Nonlinearly Elastic Composite Laminates Containing a Pin Loaded Hole." Journal of Composite Materials 18(5): 464-477. <http://hdl.handle.net/2027.42/67873>en_US
dc.identifier.issn0021-9983en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/67873
dc.description.abstractA method is presented for calculating the failure strengths and failure modes of composite laminates containing a pin loaded hole for materials exhibiting nonlinearly elastic behavior. The analysis follows that proposed by Chang, Scott, and Springer for linearly elastic composites with two notable exceptions: a) the shear stress-shear strain relation in each ply is taken to be nonlinear with the form proposed by Hahn and Tsai, and b) the Yamada-Sun failure criterion is modified to include nonlinear effects. Numerical results, generated using a nonlinear finite element scheme, were compared to data. These comparisons show that for laminates exhibiting nonlinear behavior the present analysis provides the failure strengths and failure modes more accurately than the previous method employing a linear stress-strain analysis.en_US
dc.format.extent3108 bytes
dc.format.extent525501 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.publisherSage Publicationsen_US
dc.titleFailure Strength of Nonlinearly Elastic Composite Laminates Containing a Pin Loaded Holeen_US
dc.typeArticleen_US
dc.subject.hlbsecondlevelAerospace Engineeringen_US
dc.subject.hlbtoplevelEngineeringen_US
dc.description.peerreviewedPeer Revieweden_US
dc.contributor.affiliationumDepartment of Mechanical Engineering and Applied Mechanics The University of Michigan, Ann Arbor, Michigan 48109en_US
dc.contributor.affiliationumDepartment of Mechanical Engineering and Applied Mechanics The University of Michigan, Ann Arbor, Michigan 48109en_US
dc.contributor.affiliationotherDepartment of Aeronautics and Astronautics Stanford University, Stanford, California 94305en_US
dc.description.bitstreamurlhttp://deepblue.lib.umich.edu/bitstream/2027.42/67873/2/10.1177_002199838401800506.pdf
dc.identifier.doi10.1177/002199838401800506en_US
dc.identifier.sourceJournal of Composite Materialsen_US
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dc.owningcollnameInterdisciplinary and Peer-Reviewed


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