Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum

The influence of temper condition on the tensile and compressive stress-strain behavior for six boron-aluminum laminates was investigated. In addition to monotonic tension and compression tests, tension-tension, compression-compression, and tension-compression tests were conducted to study the effec...

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Main Author: Kennedy, John M.
Other Authors: Engineering Mechanics
Format: Others
Language:en_US
Published: Virginia Polytechnic Institute and State University 2015
Subjects:
Online Access:http://hdl.handle.net/10919/54865
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spelling ndltd-VTETD-oai-vtechworks.lib.vt.edu-10919-548652021-01-07T05:32:11Z Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum Kennedy, John M. Engineering Mechanics LD5655.V855 1977.K455 Strains and stresses Tempering Aluminum The influence of temper condition on the tensile and compressive stress-strain behavior for six boron-aluminum laminates was investigated. In addition to monotonic tension and compression tests, tension-tension, compression-compression, and tension-compression tests were conducted to study the effects of cyclic loading. The laminates studied were [0], [90], [±45]<sub>S</sub>, [0/±45/0]<sub>S</sub>, [0/±45]<sub>S</sub>, and [±45/0]<sub>S</sub>, and the temper conditions were "as received" or F, T6 and T6N which was T6 followed by cryogenic exposure. It is shown that the T6 heat treatment increases the yield stress in both tension and compression. Tensile strength results are a function of the laminate configuration; unidirectional laminates were affected considerably more than other laminates with some strength values increasing and others decreasing. In general, cryogenic exposure of laminates with 0° plies increased the tensile yield stress and reduced the compressive yield stress, but other laminates were not significantly affected. Results from the cyclic tests show that the linear range of material behavior was increased by cyclic loading to a maximum value for all laminates and temper conditions. Typically, a maximum linear range was established which remained constant except in those cases where material degradation was indicated. Only those laminates with ±45° plies exhibited significant material degradation. Master of Science 2015-07-28T20:42:17Z 2015-07-28T20:42:17Z 1977 Thesis Text http://hdl.handle.net/10919/54865 en_US OCLC# 21387098 In Copyright http://rightsstatements.org/vocab/InC/1.0/ xv, 156 leaves application/pdf application/pdf Virginia Polytechnic Institute and State University
collection NDLTD
language en_US
format Others
sources NDLTD
topic LD5655.V855 1977.K455
Strains and stresses
Tempering
Aluminum
spellingShingle LD5655.V855 1977.K455
Strains and stresses
Tempering
Aluminum
Kennedy, John M.
Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
description The influence of temper condition on the tensile and compressive stress-strain behavior for six boron-aluminum laminates was investigated. In addition to monotonic tension and compression tests, tension-tension, compression-compression, and tension-compression tests were conducted to study the effects of cyclic loading. The laminates studied were [0], [90], [±45]<sub>S</sub>, [0/±45/0]<sub>S</sub>, [0/±45]<sub>S</sub>, and [±45/0]<sub>S</sub>, and the temper conditions were "as received" or F, T6 and T6N which was T6 followed by cryogenic exposure. It is shown that the T6 heat treatment increases the yield stress in both tension and compression. Tensile strength results are a function of the laminate configuration; unidirectional laminates were affected considerably more than other laminates with some strength values increasing and others decreasing. In general, cryogenic exposure of laminates with 0° plies increased the tensile yield stress and reduced the compressive yield stress, but other laminates were not significantly affected. Results from the cyclic tests show that the linear range of material behavior was increased by cyclic loading to a maximum value for all laminates and temper conditions. Typically, a maximum linear range was established which remained constant except in those cases where material degradation was indicated. Only those laminates with ±45° plies exhibited significant material degradation. === Master of Science
author2 Engineering Mechanics
author_facet Engineering Mechanics
Kennedy, John M.
author Kennedy, John M.
author_sort Kennedy, John M.
title Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
title_short Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
title_full Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
title_fullStr Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
title_full_unstemmed Influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
title_sort influence of temper condition on the nonlinear stress-strain behavior of boron-aluminum
publisher Virginia Polytechnic Institute and State University
publishDate 2015
url http://hdl.handle.net/10919/54865
work_keys_str_mv AT kennedyjohnm influenceoftemperconditiononthenonlinearstressstrainbehaviorofboronaluminum
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