Materials Guide
Aluminum Alloy Composition and Property Tables
This reference compares five common wrought aluminum alloys: 1050, 2024, 5052, 6063, and 7075. The tables list magnesium, silicon, manganese, copper, chromium,...
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Aluminum-alloy microstructures depend on composition, casting or working history, and heat treatment. This reference describes characteristic phases in cast Al-Si, Al-Cu, Al-Mg, and Al-Zn alloys and in wrought commercial-purity, corrosion-resistant, duralumin, super-duralumin, and forging alloys. It identifies eutectic silicon, alpha and beta phases, intermetallic compounds, principal strengthening phases, impurity phases, and incipient-melting features, while explaining how alloying ratios and phase morphology affect strength, ductility, corrosion resistance, heat resistance, and processability. The article preserves the source’s reported process conditions, material designations, units, and technical relationships for practical engineering reference.
The silicon mass fraction wSi is generally 5%-13%. These hypoeutectic and eutectic alloys cannot be strengthened by heat treatment. A simple binary Al-Si eutectic alloy such as ZL102 has an α + Si eutectic structure in the as-cast condition. Silicon appears as coarse needles and polygons. Modification with sodium salts, phosphorus, or other elements refines the coarse eutectic silicon and improves mechanical properties and machinability.
Al-Si alloys contain relatively few strengthening elements, and their quenching temperature is far from the eutectic point, so overheating is uncommon during solution treatment. If an excessive solution temperature causes incipient melting, the structure develops remelted globules, grain-boundary melting, and agglomerated, coarsened silicon.
The copper mass fraction wCu is 4%-11%. These alloys can be strengthened by heat treatment, principally through the θ phase, Al2Cu. Small magnesium and zinc additions can form the S phase, Al2CuMg, or T phase, AlCuZn, for supplementary strengthening. High mechanical properties at room and elevated temperatures make this system a basis for high-strength, heat-resistant cast aluminum alloys.
Al-Mg alloys have the lowest density and highest corrosion resistance among aluminum alloys, particularly against electrochemical corrosion. In the quenched condition, the structure is single-phase α. If Mg2Si is present, its lower electrode potential makes it anodic to α, so Mg2Si is continually consumed during electrochemical corrosion until a single-phase α surface remains and corrosion stops. These alloys have poor castability, a complex melting process, and low hot strength. High-magnesium grades may become brittle during long service, limiting their use.
In the as-cast condition, phases include α, silicon, Mg2Si, and a small amount of harmful black needle-like β phase, Al9Si2Fe2. Mg2Si is often difficult to observe because of its low content.

The aluminum mass fraction wAl in commercially pure aluminum is generally 98.80%-99.99%; iron and silicon form the principal impurity phases. At low iron and silicon contents, silicon dissolves in the matrix and iron forms needle-like or fine-strip Al3Fe. At higher contents, ternary compounds form. If iron exceeds silicon, an irregular plate-like or skeletal α phase, Al12Fe3Si, forms. If silicon exceeds iron, needle-like or fine-strip β phase, Al9Si2Fe2, forms.
Corrosion-resistant aluminum comprises Al-Mn and Al-Mg alloy systems.
A common grade is 3A21, with manganese as the principal addition. When wMn > 1.6%, abundant brittle Al6Mn compounds make the alloy prone to cracking during deformation. In addition to α solid solution and Al6Mn, phases may include Al6(FeMn), T(Al2Mn3Si2), α(Al12Fe3Si), and β(Al9Si2Fe2).
After annealing, an Al-Mg alloy with wMg < 2% is a single-phase α solid solution. As magnesium increases, β(Al8Mg5) appears. Above 5% Mg, the structure consists of α + β(Al8Mg5), and ductility decreases. Principal phases may include α, β(Al8Mg5), Al6Mn, Al7Cr, and Al3Ti, with impurity phases such as Al3Fe, (FeMn)Al6, and Mg2Si. The β phase in the eutectic is skeletal and appears light gray before etching.
Duralumin alloys are heat-treatable and include the Al-Cu-Mg and Al-Cu-Mn systems.
At the aluminum-rich corner of the equilibrium Al-Cu-Mg ternary diagram, solidification can produce S(Al2CuMg), θ(Al2Cu), T(Al6CuMg4), β(Al8Mg5), and α. Actual magnesium contents are relatively low, placing alloys in the α + S, α + θ + S, or α + θ phase fields. The two principal strengthening phases are therefore θ and S.
The copper mass fraction can reach 6%-7%. Copper and aluminum form the strengthening phase Al2Cu, which strengthens the alloy after quenching and artificial aging. At wMn = 0.4%-0.5%, finely dispersed T(Al2CuMn2) improves heat resistance. Excess manganese increases and coarsens the T phase, enlarging phase boundaries and accelerating diffusion. Heat resistance then falls and hot-cracking tendency during welding increases.
Common super-duralumin alloys contain α, MgZn2, T(Al2Mg3Zn3), an α + T(Al2Mg3Zn3) eutectic, and impurity phases such as (FeMn)Al6 and Mg2Si.
Forging aluminum alloys are generally divided into two systems.
When copper is very low and the magnesium-to-silicon mass ratio is 1.73, Mg2Si forms and all copper dissolves in the matrix. At higher copper contents and a magnesium-to-silicon ratio below 1.08, ω(AlCu4Mg5Si4) can form, with the remaining copper forming θ(Al2Cu). Adding copper to Al-Mg-Si alloys can therefore introduce ω, S, and θ in addition to Mg2Si.
These alloys contain less copper and magnesium than duralumin and therefore contain more S phase, Al2CuMg. Iron and nickel form Al9FeNi, which has good thermal stability. Excess iron forms Al7Cu2Fe, while excess nickel can form AlCuNi.
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Materials Guide
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