1989
DOI: 10.1515/ijmr-1989-800307
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Mechanical Properties of Al-Mg Alloys at Elevated Temperatures / Mechanical Properties of Al-Mg Alloys at Elevated Temperatures

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Cited by 2 publications
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“…For these Al alloys, Hammad and Ramadan [51] found that increasing the strain rate in the range 5.5 × 10 −5 to 5.5 × 10 −3 s −1 decreased the hot ductility, as measured by elongation in an Al-3% Mg alloy. The alloy was solution treated and water quenched and tensile tested in the temperature range 27 to 530 • C. The high-temperature embrittlement was suggested as being due to precipitation of Al 3 Mg 2 and Mg 5 Al 3 compounds.…”
Section: Troughs In Aluminium Alloysmentioning
confidence: 94%
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“…For these Al alloys, Hammad and Ramadan [51] found that increasing the strain rate in the range 5.5 × 10 −5 to 5.5 × 10 −3 s −1 decreased the hot ductility, as measured by elongation in an Al-3% Mg alloy. The alloy was solution treated and water quenched and tensile tested in the temperature range 27 to 530 • C. The high-temperature embrittlement was suggested as being due to precipitation of Al 3 Mg 2 and Mg 5 Al 3 compounds.…”
Section: Troughs In Aluminium Alloysmentioning
confidence: 94%
“…Creep normally manifests itself when the temperature (T) > 0.3-0.4 (T m ), where T m is the melting point in • C [91]. Hence for steel, copper, aluminium, and nickel, the ratios are 0.6, with the centre of the hot-ductility troughs being at ~900, 700, 250, and 400 • C, respectively, as noted in Table 2, with the data being taken from the literature [11,27,34,35,51,56,60]. Although Al alloys can have a hot-ductility trough in the intermediate-temperature region, it is most likely that when failure occurs on tensile testing these alloys in the temperature range of the trough, it is due to one of the following: the weakening of the cohesive strength of the boundaries, the formation of liquid films, or oxygen infiltration to the grain surfaces, rather than creep cavitation.…”
Section: Strain Ratementioning
confidence: 99%
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