Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)

The impact mechanical properties of the widely used in the aeronautics A357 cast aluminum alloy were investigated by exploiting experiments on an instrumented Charpy impact testing machine. The evaluated impact properties for 25 different artificial aging heat treatment conditions were analyzed a...

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Main Author: Alexopoulos N.D.
Format: Article
Language:English
Published: EDP Sciences 2010-06-01
Series:EPJ Web of Conferences
Online Access:http://dx.doi.org/10.1051/epjconf/20100602002
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author Alexopoulos N.D.
author_facet Alexopoulos N.D.
author_sort Alexopoulos N.D.
collection DOAJ
description The impact mechanical properties of the widely used in the aeronautics A357 cast aluminum alloy were investigated by exploiting experiments on an instrumented Charpy impact testing machine. The evaluated impact properties for 25 different artificial aging heat treatment conditions were analyzed and discussed in conjunction with the respective tensile properties. Correlations are proposed to establish useful relationships between impact resistance and tensile strain energy density properties. The established correlations, which are well supported by the performed experiments, can be used to estimate the tensile ductility and toughness of the A357 cast aluminum alloy from the Charpy impact test. Performed fractographic analyses were supporting the physically arbitrary correlation between tensile strain energy density and impact resistance.
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spelling doaj.art-cdf9cc30687e4da0941abc755ae854e52022-12-21T20:07:34ZengEDP SciencesEPJ Web of Conferences2100-014X2010-06-0160200210.1051/epjconf/20100602002Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)Alexopoulos N.D.The impact mechanical properties of the widely used in the aeronautics A357 cast aluminum alloy were investigated by exploiting experiments on an instrumented Charpy impact testing machine. The evaluated impact properties for 25 different artificial aging heat treatment conditions were analyzed and discussed in conjunction with the respective tensile properties. Correlations are proposed to establish useful relationships between impact resistance and tensile strain energy density properties. The established correlations, which are well supported by the performed experiments, can be used to estimate the tensile ductility and toughness of the A357 cast aluminum alloy from the Charpy impact test. Performed fractographic analyses were supporting the physically arbitrary correlation between tensile strain energy density and impact resistance.http://dx.doi.org/10.1051/epjconf/20100602002
spellingShingle Alexopoulos N.D.
Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)
EPJ Web of Conferences
title Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)
title_full Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)
title_fullStr Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)
title_full_unstemmed Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)
title_short Impact properties of the aircraft cast aluminium alloy Al-7Si0.6Mg (A357)
title_sort impact properties of the aircraft cast aluminium alloy al 7si0 6mg a357
url http://dx.doi.org/10.1051/epjconf/20100602002
work_keys_str_mv AT alexopoulosnd impactpropertiesoftheaircraftcastaluminiumalloyal7si06mga357