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Large deflection analysis of thin elastic structures by the assumed stress hybrid finite element method.

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Large deflection analysis of thin elastic structures by the assumed stress hybrid finite element method.

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Author: Boland, Peter Lewis
Department: Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics
Publisher: Massachusetts Institute of Technology
Date Issued: 1976
Description:
Thesis. 1976. Ph.D.--Massachusetts Institute of Technology. Dept. of Aeronautics and Astronautics.Microfiche copy available in Archives and Aero.Vita.Bibliography: p.194-204.
URI: http://hdl.handle.net/1721.1/16381
Keywords: Aeronautics and Astronautics, Elastic plates and shells, Finite element method, Deformations (Mechanics), Virtual work, Strains and stresses

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