NASA NTRS · 20040070826
Thermo-Elastic Triangular Sandwich Element for the Complete Stress Field Based on a Single-Layer Theory
Abstract
This study presents a new triangular finite element for modeling thick sandwich panels, subjected to thermo-mechanical loading, based on a {3,2}-order single-layer plate theory. A hybrid energy functional is employed in the derivation of the element because of a C interelement continuity requirement. The single-layer theory is based on five weighted-average field variables arising from the cubic and quadratic representations of the in-plane and transverse displacement fields, respectively. The variations of temperature and distributed loading acting on the top and bottom surfaces are non-uniform. The temperature varies linearly through the thickness.
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Das, M., Barut, A., Madenci, E., Ambur, D. R.. 2004-01-01. Thermo-Elastic Triangular Sandwich Element for the Complete Stress Field Based on a Single-Layer Theory. https://ntrs.nasa.gov/citations/20040070826
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