Analysis and Evaluation of a Shell Finite Element with Drilling Degree of Freedom
dc.contributor.advisor | Austin, M.A. | en_US |
dc.contributor.author | Jin, Lanheng | en_US |
dc.contributor.department | ISR | en_US |
dc.date.accessioned | 2007-05-23T09:58:02Z | |
dc.date.available | 2007-05-23T09:58:02Z | |
dc.date.issued | 1994 | en_US |
dc.description.abstract | A 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.extent | 315470 bytes | |
dc.format.mimetype | application/pdf | |
dc.identifier.uri | http://hdl.handle.net/1903/5582 | |
dc.language.iso | en_US | en_US |
dc.relation.ispartofseries | ISR; MS 1994-12 | en_US |
dc.subject | computer aided design | en_US |
dc.subject | space structures | en_US |
dc.subject | Intelligent Control Systems | en_US |
dc.title | Analysis and Evaluation of a Shell Finite Element with Drilling Degree of Freedom | en_US |
dc.type | Thesis | en_US |
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