Compression Failure of Aluminum Plates Exposed to Constant Heat Flux

Aluminum is used as a structural member in marine applications because of its low weight. One challenge is to design against failure of aluminum structures in fire. A parametric study was performed to quantify the effects of parameters on the compression failure of aluminum plates during a fire....

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Main Author: Fogle, Emily Johanna
Other Authors: Mechanical Engineering
Format: Others
Published: Virginia Tech 2014
Subjects:
Online Access:http://hdl.handle.net/10919/33011
http://scholar.lib.vt.edu/theses/available/etd-05192010-154237/
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-330112020-09-26T05:37:22Z Compression Failure of Aluminum Plates Exposed to Constant Heat Flux Fogle, Emily Johanna Mechanical Engineering Lattimer, Brian Y. West, Robert L. Jr. Case, Scott W. compression loading intermediate-scale fire Aluminum is used as a structural member in marine applications because of its low weight. One challenge is to design against failure of aluminum structures in fire. A parametric study was performed to quantify the effects of parameters on the compression failure of aluminum plates during a fire. A thermo-structural apparatus was designed to perform compression tests on aluminum samples consisting of a compression load frame, a hydraulic system, and electric heaters. The effect of dimensional variation on failure behavior was examined. Aluminum 5083 and 6082 alloys were tested with three thicknesses, two lengths and two widths. Three heat fluxes and various buckling stresses were used. Micro Vickerâ s hardness values were measured before and after testing to quantify the effect of heating on the strength of the aluminum. In general, lower applied stress resulted in higher failure temperature and longer time to failure. Dimensional variations had a negligible effect on failure behavior. The 5083 alloy has a minimum stress level of 50% of the buckling stress at 10kW/m2 and 10% of the buckling stress at 20kW/m2, while the 6082 alloy has a minimum stress level of 75% of the buckling stress at 10kW/m2 and 25% of the buckling stress at 20kW/m2. The 6082 failed at higher temperatures and longer failure times than the 5083. The presence of insulation on the exposed surface decreased the temperature rise, resulting in longer failure times. Vickerâ s hardness decreased with heating in general. The results describe the effects of parameters of the failure of aluminum. Master of Science 2014-03-14T20:37:41Z 2014-03-14T20:37:41Z 2010-05-05 2010-05-19 2010-06-01 2010-06-01 Thesis etd-05192010-154237 http://hdl.handle.net/10919/33011 http://scholar.lib.vt.edu/theses/available/etd-05192010-154237/ Fogle_EJ_T_2010.pdf In Copyright http://rightsstatements.org/vocab/InC/1.0/ application/pdf Virginia Tech
collection NDLTD
format Others
sources NDLTD
topic compression loading
intermediate-scale
fire
spellingShingle compression loading
intermediate-scale
fire
Fogle, Emily Johanna
Compression Failure of Aluminum Plates Exposed to Constant Heat Flux
description Aluminum is used as a structural member in marine applications because of its low weight. One challenge is to design against failure of aluminum structures in fire. A parametric study was performed to quantify the effects of parameters on the compression failure of aluminum plates during a fire. A thermo-structural apparatus was designed to perform compression tests on aluminum samples consisting of a compression load frame, a hydraulic system, and electric heaters. The effect of dimensional variation on failure behavior was examined. Aluminum 5083 and 6082 alloys were tested with three thicknesses, two lengths and two widths. Three heat fluxes and various buckling stresses were used. Micro Vickerâ s hardness values were measured before and after testing to quantify the effect of heating on the strength of the aluminum. In general, lower applied stress resulted in higher failure temperature and longer time to failure. Dimensional variations had a negligible effect on failure behavior. The 5083 alloy has a minimum stress level of 50% of the buckling stress at 10kW/m2 and 10% of the buckling stress at 20kW/m2, while the 6082 alloy has a minimum stress level of 75% of the buckling stress at 10kW/m2 and 25% of the buckling stress at 20kW/m2. The 6082 failed at higher temperatures and longer failure times than the 5083. The presence of insulation on the exposed surface decreased the temperature rise, resulting in longer failure times. Vickerâ s hardness decreased with heating in general. The results describe the effects of parameters of the failure of aluminum. === Master of Science
author2 Mechanical Engineering
author_facet Mechanical Engineering
Fogle, Emily Johanna
author Fogle, Emily Johanna
author_sort Fogle, Emily Johanna
title Compression Failure of Aluminum Plates Exposed to Constant Heat Flux
title_short Compression Failure of Aluminum Plates Exposed to Constant Heat Flux
title_full Compression Failure of Aluminum Plates Exposed to Constant Heat Flux
title_fullStr Compression Failure of Aluminum Plates Exposed to Constant Heat Flux
title_full_unstemmed Compression Failure of Aluminum Plates Exposed to Constant Heat Flux
title_sort compression failure of aluminum plates exposed to constant heat flux
publisher Virginia Tech
publishDate 2014
url http://hdl.handle.net/10919/33011
http://scholar.lib.vt.edu/theses/available/etd-05192010-154237/
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