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NASA NTRS · 20040077262

Elasto-Plastic Analysis of Tee Joints Using HOT-SMAC

Abstract

The Higher Order Theory - Structural/Micro Analysis Code (HOT-SMAC) software package is applied to analyze the linearly elastic and elasto-plastic response of adhesively bonded tee joints. Joints of this type are finding an increasing number of applications with the increased use of composite materials within advanced aerospace vehicles, and improved tools for the design and analysis of these joints are needed. The linearly elastic results of the code are validated vs. finite element analysis results from the literature under different loading and boundary conditions, and new results are generated to investigate the inelastic behavior of the tee joint. The comparison with the finite element results indicates that HOT-SMAC is an efficient and accurate alternative to the finite element method and has a great deal of potential as an analysis tool for a wide range of bonded joints.

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BibTeXRIS

Arnold, Steve M., Bednarcyk, Brett A., Yarrington, Phillip W.. 2004-05-01. Elasto-Plastic Analysis of Tee Joints Using HOT-SMAC. https://ntrs.nasa.gov/citations/20040077262

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