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Thermo-Elastic Triangular Sandwich Element for the Complete Stress Field Based on a Single-Layer TheoryThis 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.
Document ID
20040070826
Acquisition Source
Langley Research Center
Document Type
Conference Paper
Authors
Das, M.
(Arizona Univ. Tucson, AZ, United States)
Barut, A.
(Arizona Univ. Tucson, AZ, United States)
Madenci, E.
(Arizona Univ. Tucson, AZ, United States)
Ambur, D. R.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2004
Subject Category
Structural Mechanics
Report/Patent Number
AIAA Paper 2004-1770
Report Number: AIAA Paper 2004-1770
Meeting Information
Meeting: 45th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference
Location: Palm Springs, CA
Country: United States
Start Date: April 19, 2004
End Date: April 22, 2004
Sponsors: American Society of Civil Engineers, American Helicopter Society, Inc., American Society of Mechanical Engineers, American Society for Composites, American Inst. of Aeronautics and Astronautics
Funding Number(s)
OTHER: 23-762-55-LE
Distribution Limits
Public
Copyright
Public Use Permitted.
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