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dc.rights.licenseRestricted to current Rensselaer faculty, staff and students. Access inquiries may be directed to the Rensselaer Libraries.
dc.contributorGoetschel, Daniel
dc.contributor.authorCackett, Matthew Thomas
dc.date.accessioned2021-11-03T08:42:11Z
dc.date.available2021-11-03T08:42:11Z
dc.date.created2016-11-01T11:26:26Z
dc.date.issued1983-08
dc.identifier.urihttps://hdl.handle.net/20.500.13015/1814
dc.descriptionAugust 1983
dc.descriptionSchool of Engineering
dc.description.abstractGeneral design considerations for pin-loaded holes in orthotropic plates are reported. As a specific design case, the pinned lug connection on the drag-strut of the Lockheed L-10ll was redesigned using Hy-E 1046 AE graphite/epoxy. Six proposed designs were manufactured and tested for ultimate tensile strength. Failure analysis was performed using a new variation of the Whitney-Nuismer stress averaging technique in conjunction with finite element modeling. Correlation between predicted strength and experimental strength was found to be good and is compared with other failure models. Parametric studies of geometry and material variation were performed for the pinned lug case.
dc.language.isoENG
dc.publisherRensselaer Polytechnic Institute, Troy, NY
dc.relation.ispartofRensselaer Theses and Dissertations Online Collection
dc.subjectMechanical engineering
dc.titleThe design considerations and failure analysis of a pin-loaded hole in an orthotrophic laminate
dc.typeElectronic thesis
dc.typeThesis
dc.digitool.pid177705
dc.digitool.pid177706
dc.digitool.pid177708
dc.digitool.pid177707
dc.digitool.pid177709
dc.rights.holderThis electronic version is a licensed copy owned by Rensselaer Polytechnic Institute, Troy, NY. Copyright of original work retained by author.
dc.description.degreeMS
dc.relation.departmentDept. of Mechanical Engineering


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