TECHNICAL PAPERS
Sep 22, 2010

Structural Analysis of Compression Deformation and Failure of Aluminum in Fire

Publication: Journal of Structural Engineering
Volume 137, Issue 7

Abstract

This paper presents a finite-element (FE) modeling approach to predict the deformation, softening, and failure of compression-loaded aluminum structures exposed to fire. A fully coupled thermal-mechanical FE model is outlined. The FE model can analyze the thermal profile and deformation as well as the initial and final plastic collapse of aluminum structures in fire. It calculates the temperature profile of an aluminum structure exposed to unsteady-state heating conditions representative of fire. Using the temperature profile, the elastic and plastic deformations together with the loss in the compression load capacity of an aluminum structure caused by elastic softening, time-independent plastic (yield) softening, and time-dependent plastic (creep) softening effects are analyzed by using a mechanics-based FE solution. The modeling approach is validated by structural tests on an aluminum alloy (5083 Al) plate supporting an applied compression load while locally heated at different radiant heat flux (temperature) levels. The modeling approach can estimate the deformations, initiation of plastic collapse, and final failure of the aluminum test article for heat flux levels representative of different fire types. The FE model described in this paper can be used as the basis for performing complex deformation and failure analysis of compression-loaded aluminum (and other metallic) structures in fire.

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Acknowledgments

This research was performed as part of a research project (P2.1.3) within the Cooperative Research Centre for Advanced Composite Structures (CRC-ACS Ltd). The study was funded by the U.S. Office of Naval Research (Grant No. UNSPECIFIEDN00014-07010514) under the direction of Dr. L. Couchman. The authors thank Peter Tkatchyk of Royal Melbourne Institute of Technology (RMIT) for constructing the fire-under-load test apparatus and for technical assistance in the experimental testing.

References

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Published In

Go to Journal of Structural Engineering
Journal of Structural Engineering
Volume 137Issue 7July 2011
Pages: 728 - 738

History

Received: Mar 10, 2010
Accepted: Sep 12, 2010
Published online: Sep 22, 2010
Published in print: Jul 1, 2011

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Authors

Affiliations

S. Feih
School of Aerospace, Mechanical, and Manufacturing Engineering, RMIT Univ., GPO Box 2476, Melbourne, Australia; and Cooperative Research Centre for Advanced Composite Structures Ltd. (CRC-ACS), 506 Lorimer St., Fishermans Bend, Victoria, Australia.
E. Kandare
School of Aerospace, Mechanical, and Manufacturing Engineering, RMIT Univ., GPO Box 2476, Melbourne, Australia; and Cooperative Research Centre for Advanced Composite Structures Ltd. (CRC-ACS), 506 Lorimer St., Fishermans Bend, Victoria, Australia.
B. Y. Lattimer
Dept. of Mechanical Engineering, Virginia Polytechnic Institute and State University, Blacksburg, VA 24061.
A. P. Mouritz [email protected]
School of Aerospace, Mechanical, and Manufacturing Engineering, RMIT Univ., GPO Box 2476, Melbourne, Australia (corresponding author). E-mail: [email protected]

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