Toughness-strength relations in the overaged 7449 Al-Based alloy
Kamp, N., Sinclair, I. and Starink, M.J. (2002) Toughness-strength relations in the overaged 7449 Al-Based alloy. Metallurgical and Materials Transactions A, 33, (4), 1125-1136. (doi:10.1007/s11661-002-0214-2).
- Version of Record
This article examines the relationship between plane strain fracture toughness, KIc, the tensile properties, and the microstructure of the overaged 7449 aluminum-plate alloy, and compares them to the 7150 alloy. The 7449 alloy has a higher content of η′/η precipitates; and, the 7150 alloy contains a greater amount of coarse intermetallic particles, as it contains an appreciable amount of coarse S phase (Al2CuMg), which is largely absent in the 7449 alloy. The toughness of the alloys shows an increase on overaging, and the 7449 alloy shows a reasonably linear toughness—yield strength relation on extended overaging. Several mechanisms of failure occur: coarse voiding at intermetallics and a combined intergranular/transgranular shear fracture mode, with the former becoming more important as overaging progresses. Drawbacks of existing models for toughness are discussed, and a new model for plane strain fracture toughness, based on the microstructurally dependent work-hardening factor, KA, introduced in Ashby's theory of work hardening, is developed. This model predicts a linear relation between KIc and K0.85A/σ0.35ys, where σys is the yield strength, which is consistent with the experimental data.
|Digital Object Identifier (DOI):||doi:10.1007/s11661-002-0214-2|
|Subjects:||T Technology > TJ Mechanical engineering and machinery
T Technology > TL Motor vehicles. Aeronautics. Astronautics
|Divisions:||University Structure - Pre August 2011 > School of Engineering Sciences
University Structure - Pre August 2011 > School of Engineering Sciences > Engineering Materials & Surface Engineering
|Date Deposited:||16 Mar 2006|
|Last Modified:||31 Mar 2015 11:08|
|RDF:||RDF+N-Triples, RDF+N3, RDF+XML, Browse.|
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