Analysis and Evaluation of a Shell Finite Element with Drilling Degree of Freedom

dc.contributor.advisorAustin, M.A.en_US
dc.contributor.authorJin, Lanhengen_US
dc.contributor.departmentISRen_US
dc.date.accessioned2007-05-23T09:58:02Z
dc.date.available2007-05-23T09:58:02Z
dc.date.issued1994en_US
dc.description.abstractA flat shell finite element is obtained by superposing plate bending and membrane components. Normally, shell elements of this type possess five degrees of freedom (DOF), three displacement DOF, u, v and w, and two in-plane rotation DOF, qx and qy , at each node. A sixth degree of freedom, qz , is associated with the shell normal rotation, and is not usually required by the theory. In practice, however, computational and modeling problems can be caused by a failure to include this degree of freedom in finite element models.<P>This paper presents the formulation and testing of a four node quadrilateral thin flat shell finite element, which has six DOF per node. The sixth DOF is obtained by combining by a membrane element with a normal rotation qz, the so-called the drilling degree of freedom, and a discrete Kirchhoff plate element. The flat shell has a 24 x 24 element stiffness matrix. Numerical examples are given for (a) shear- loaded cantilever beam, (b) square plate, (c) cantilever I- beam and (d) folded plate.en_US
dc.format.extent315470 bytes
dc.format.mimetypeapplication/pdf
dc.identifier.urihttp://hdl.handle.net/1903/5582
dc.language.isoen_USen_US
dc.relation.ispartofseriesISR; MS 1994-12en_US
dc.subjectcomputer aided designen_US
dc.subjectspace structuresen_US
dc.subjectIntelligent Control Systemsen_US
dc.titleAnalysis and Evaluation of a Shell Finite Element with Drilling Degree of Freedomen_US
dc.typeThesisen_US

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