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Failure of Composite Laminates Containing Pin Loaded Holes—Method of Solution
dc.contributor.authorChang, Fu-Kuoen_US
dc.contributor.authorScott, Richarden_US
dc.contributor.authorSpringer, George S.en_US
dc.date.accessioned2010-04-13T19:59:59Z
dc.date.available2010-04-13T19:59:59Z
dc.date.issued1984en_US
dc.identifier.citationChang, Fu-Kuo; Scott, Richard; Springer, George (1984). "Failure of Composite Laminates Containing Pin Loaded Holes—Method of Solution." Journal of Composite Materials 18(3): 255-278. <http://hdl.handle.net/2027.42/67981>en_US
dc.identifier.issn0021-9983en_US
dc.identifier.urihttps://hdl.handle.net/2027.42/67981
dc.description.abstractA method is presented for predicting the failure strength and the failure mode of fiber reinforced composite laminates containing one or two pin loaded holes. The method involves two steps. First, the stress distribution in the laminate is calculated by the use of a finite element method. Second, the failure load and failure mode are predicted by means of a proposed failure hypothesis together with the Yamada-Sun failure criterion. A computer code was developed which can be used to calculate the maximum load and the mode of failure of laminates with different ply orientations, different material properties, and different geometries. Tests were also conducted measuring the failure strengths and failure modes of Fiberite T300/1034-C laminates containing a pin-loaded hole or two pin-loaded holes in parallel or in series. Com parisons were made between the data and the results of the model. Good agreement was found between the analytical and the experimental results.en_US
dc.format.extent3108 bytes
dc.format.extent928529 bytes
dc.format.mimetypetext/plain
dc.format.mimetypeapplication/pdf
dc.publisherSage Publicationsen_US
dc.titleFailure of Composite Laminates Containing Pin Loaded Holes—Method of Solutionen_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/2027.42/67981/2/10.1177_002199838401800305.pdf
dc.identifier.doi10.1177/002199838401800305en_US
dc.identifier.sourceJournal of Composite Materialsen_US
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dc.identifier.citedreference. Chang, F.K., Scott, R.A., and Springer, G.S., "Failure Strength of Nonlinearly Elastic Composite Laminates Containing a Pin Loaded Hole," J. of Composite Materials, Vol. 18, pp. 255-278 (1984).en_US
dc.owningcollnameInterdisciplinary and Peer-Reviewed


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