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Effect of solution treatment on the strength and fracture toughness of aluminum alloy 7050

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TLDR
In this article, the effect of the solution treatment on the tensile property and fracture toughness of aluminum alloy 7050 were investigated by means of optical microscopy, scanning electron microscopy (SEM), transmission electron microscope (TEM), tensile test and the plane-strain fracture toughness test.
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This article is published in Journal of Alloys and Compounds.The article was published on 2011-03-10. It has received 128 citations till now. The article focuses on the topics: Fracture toughness & Ultimate tensile strength.

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Effects of Sc and Zr microalloying additions on the microstructure and mechanical properties of new Al–Zn–Mg alloys

TL;DR: In this article, the effects of Sc and Zr microalloying additions on the microstructure and mechanical properties of new Al-Zn-Mg alloys alloyed with a small amount of copper were investigated by tensile tests and microscopy methods.
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The effect of quench rate and overageing temper on the corrosion behaviour of AA7050

TL;DR: In this article, the corrosion behavior of AA7050 on different quench rates and ageing conditions has been studied using immersion tests and complementary techniques like SEM, TEM-EDS and Scanning Kelvin probe force microscopy.
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Flow behavior modeling of the 7050 aluminum alloy at elevated temperatures considering the compensation of strain

TL;DR: In this article, a constitutive equation of 7050 aluminum alloy considering the compensation of the strain was proposed, and the correlation coefficient and the average absolute relative error (AARE) were introduced to verify the validity of the constitutive equations.
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Effect of post weld heat treatment on tensile properties and microstructure characteristics of friction stir welded armour grade AA7075-T651 aluminium alloy

TL;DR: In this article, the effects of post weld heat treatments, namely artificial ageing and solution treatment followed by artificial ageing, on microstructure and mechanical properties of 12mm thick friction stir welded joints of precipitation hardenable high strength armour grade AA7075-T651 aluminium alloy.
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Influence of heat treatment on the strength and fracture toughness of 7N01 aluminum alloy

TL;DR: In this article, the microstructures of 7N01 aluminum alloys were investigated using optical microscopy (OM), transmission electron microscopy, and scanning electron microscope (SEM) images.
References
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Journal ArticleDOI

Application of modern aluminum alloys to aircraft

TL;DR: Aluminum alloys have been the primary material of choice for structural components of aircraft since about 1930 as discussed by the authors and have been used extensively in high-performance military aircraft and are being specified for some applications in modern commercial aircraft, including the fuselage, wing, and supporting structure of commercial airliners and military cargo and transport.
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Recent development in aluminium alloys for aerospace applications

TL;DR: In this article, the authors investigated new processing routes and new alloy chemistries for aircraft materials, which offer major improvements in ductility, toughness, fatigue performance and in reduction of residual stress in large dimension plate and sheet products.
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Structure-property correlations in Al 7050 and Al 7055 high-strength aluminum alloys

TL;DR: In this article, the information available from different studies conducted on alloys Al 7050 and Al 7055 was collated to prepare maps that are intended to serve as guides to design aluminum alloys with desired combination of properties.
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Overview no. 102 Theory assisted design of high strength low alloy aluminum

TL;DR: The design of an aluminum alloy having good strength while maintaining a high resistance to fracture is discussed in this article, where the desired microstructure consists of a small volume fraction of an ultra-fine dispersion of hard particles.
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Effect of a short solution treatment time on microstructure and mechanical properties of modified Al–7wt.%Si–0.3wt.%Mg alloy

TL;DR: In this article, the impact energy of a strontium modified Al-7wt.%Si−0.3%Mg cast alloy was studied and it was found that a solution treatment of 10 min at 540 or 550 °C is sufficient for the α-aluminium phase to homogenise and achieve the maximum level of magnesium and silicon as predicted by the solubility and alloy composition limits.
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