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2D Finite Element Formulation for 3D Temperature Analysis of Layered Hybrid Structures

Rolfes, R. and Tessmer, J. (2001) 2D Finite Element Formulation for 3D Temperature Analysis of Layered Hybrid Structures. In: Seminar: Numerical Simulation of Heat Transfer, pp. 1-5. NAFEMS-Seminar: "Numerical Simulation of Heat Transfer", Wiesbaden, 9./10.5.2001.

Full text not available from this repository.

Abstract

Three-dimensional (3D) finite element formulations are usually applied for the analysis of temperature fields for hybrid and conventional composite structures. This leads to a high effort with respect to discretisation and computation time, especially for transient calculations. Using a new formulation basing on a two-dimensional (2D) finite element discretisation it is now possible to approximate the three-dimensional temperature field very effectively. Through combination of layerwise shape functions in thickness direction (linear or quadratic) and suitable heat transfer conditions at the interfaces the nodal number of degrees of freedom remains independent from the number of layers. In conjunction with shell elements that are generally applied for the stress analysis of thin composite structures it is also easier to transfer temperature data fields due to the same two-dimensional discretisation. This leads to a fast and accurate formulation for the temperature analysis of hybrid composite structures.

Document Type:Conference or Workshop Item (Paper)
Additional Information: LIDO-Berichtsjahr=2001, monograph_id=5,
Title:2D Finite Element Formulation for 3D Temperature Analysis of Layered Hybrid Structures
Authors:
AuthorsInstitution or Email of Authors
Rolfes, R.UNSPECIFIED
Tessmer, J.UNSPECIFIED
Date:2001
Journal or Publication Title:Seminar: Numerical Simulation of Heat Transfer
Page Range:pp. 1-5
Editors:
EditorsEmail
Nafems, UNSPECIFIED
Status:Published
Keywords:Finite elements; thermal analysis; hybrid composite structures; layerwise theory
Event Title:NAFEMS-Seminar: "Numerical Simulation of Heat Transfer", Wiesbaden, 9./10.5.2001
Organizer:NAFEMS
HGF - Research field:Aeronautics, Space and Transport (old)
HGF - Program:Aeronautics
HGF - Program Themes:other
DLR - Research area:Aeronautics
DLR - Program:L ST - Starrflüglertechnologien
DLR - Research theme (Project):UNSPECIFIED
Location: Braunschweig
Institutes and Institutions:Institute of Composite Structures and Adaptive Systems > Institut für Strukturmechanik
Deposited By: Sibylle Wolff
Deposited On:16 Sep 2005
Last Modified:14 Jan 2010 16:08

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