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dc.contributor.advisorHaisler, Walter E.
dc.contributor.advisorStricklin, James A.
dc.creatorHunsaker, Barry
dc.date.accessioned2020-08-21T22:00:55Z
dc.date.available2020-08-21T22:00:55Z
dc.date.issued1976
dc.identifier.urihttps://hdl.handle.net/1969.1/DISSERTATIONS-614527
dc.descriptionVita.en
dc.description.abstractFirst, the continuum equations of motion are referred to the initial structural configuration and then linearized with respect to the displacement increments to obtain a form of the so-called total Lagrangian formulation whose kinematics are valid for large strains. These equations are then converted to a set of nonlinear differential equations via the finite element method. The formulation and computational procedures of two incremental plasticity theory hardening rules, namely combined kinematic-isotropic hardening and the mechanical sublayer model, are then presented with the limitation of small strains. Of particular interest is a new method of determining sublayer parameters of the mechanical sublayer model applicable to multiaxial loading. Finally, three simple structures subjected to loading into the plastic range are analyzed using the finite element code AGGIE I.en
dc.format.extentviii, 86 leaves ;en
dc.format.mediumelectronicen
dc.format.mimetypeapplication/pdf
dc.language.isoeng
dc.rightsThis thesis was part of a retrospective digitization project authorized by the Texas A&M University Libraries. Copyright remains vested with the author(s). It is the user's responsibility to secure permission from the copyright holder(s) for re-use of the work beyond the provision of Fair Use.en
dc.rights.urihttp://rightsstatements.org/vocab/InC/1.0/
dc.subjectFinite element methoden
dc.subjectPlasticityen
dc.subjectStrain hardeningen
dc.subjectAerospace Engineeringen
dc.subject.classification1976 Dissertation H938
dc.subject.lcshPlasticityen
dc.subject.lcshStrain hardeningen
dc.subject.lcshFinite element methoden
dc.titleThe application of combined kinematic-isotropic hardening and the mechanical sublayer model to small strain inelastic structural analysis by the finite element methoden
dc.typeThesisen
thesis.degree.grantorTexas A&M Universityen
thesis.degree.nameDoctor of Philosophyen
dc.contributor.committeeMemberCoonwell, L. R.
dc.type.genredissertationsen
dc.type.materialtexten
dc.format.digitalOriginreformatted digitalen
dc.publisher.digitalTexas A&M University. Libraries
dc.identifier.oclc2697595


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