A new stiffened shell element for geometrically nonlinear analysis of composite laminates

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Keywords: Composite; Finite element; Nonlinear; Stiffened shell

Document Type: Research Article

DOI: http://dx.doi.org/10.1016/S0045-7949(99)00201-1

Affiliations: aDepartment of Aerospace and Mechanical Engineering, The University of Arizona, Aero Building 16, Tucson, AZ, USA

Publication date: June 1, 2000

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