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1050A Aluminum vs. 332.0 Aluminum

Both 1050A aluminum and 332.0 aluminum are aluminum alloys. They have 85% of their average alloy composition in common.

For each property being compared, the top bar is 1050A aluminum and the bottom bar is 332.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 20 to 45
110
Elastic (Young's, Tensile) Modulus, GPa 68
73
Elongation at Break, % 1.1 to 33
1.0
Fatigue Strength, MPa 22 to 55
90
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
27
Shear Strength, MPa 44 to 97
190
Tensile Strength: Ultimate (UTS), MPa 68 to 170
250
Tensile Strength: Yield (Proof), MPa 22 to 150
190

Thermal Properties

Latent Heat of Fusion, J/g 400
530
Maximum Temperature: Mechanical, °C 170
170
Melting Completion (Liquidus), °C 660
580
Melting Onset (Solidus), °C 650
530
Specific Heat Capacity, J/kg-K 900
880
Thermal Conductivity, W/m-K 230
100
Thermal Expansion, µm/m-K 24
21

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 59
26
Electrical Conductivity: Equal Weight (Specific), % IACS 200
84

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
10
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 8.2
7.8
Embodied Energy, MJ/kg 150
140
Embodied Water, L/kg 1200
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.9 to 19
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 3.7 to 160
250
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 50
50
Strength to Weight: Axial, points 6.9 to 18
24
Strength to Weight: Bending, points 14 to 25
31
Thermal Diffusivity, mm2/s 94
42
Thermal Shock Resistance, points 3.0 to 7.6
12

Alloy Composition

Aluminum (Al), % 99.5 to 100
80.1 to 89
Copper (Cu), % 0 to 0.050
2.0 to 4.0
Iron (Fe), % 0 to 0.4
0 to 1.2
Magnesium (Mg), % 0 to 0.050
0.5 to 1.5
Manganese (Mn), % 0 to 0.050
0 to 0.5
Nickel (Ni), % 0
0 to 0.5
Silicon (Si), % 0 to 0.25
8.5 to 10.5
Titanium (Ti), % 0 to 0.050
0 to 0.25
Zinc (Zn), % 0 to 0.070
0 to 1.0
Residuals, % 0
0 to 0.5