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772.0 Aluminum vs. 240.0 Aluminum

Both 772.0 aluminum and 240.0 aluminum are aluminum alloys. They have 85% of their average alloy composition in common.

For each property being compared, the top bar is 772.0 aluminum and the bottom bar is 240.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
72
Elongation at Break, % 6.3 to 8.4
1.0
Fatigue Strength, MPa 94 to 160
140
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 26
27
Tensile Strength: Ultimate (UTS), MPa 260 to 320
240
Tensile Strength: Yield (Proof), MPa 220 to 250
200

Thermal Properties

Latent Heat of Fusion, J/g 380
380
Maximum Temperature: Mechanical, °C 180
180
Melting Completion (Liquidus), °C 630
600
Melting Onset (Solidus), °C 580
520
Specific Heat Capacity, J/kg-K 870
860
Thermal Conductivity, W/m-K 150
96
Thermal Expansion, µm/m-K 24
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
23
Electrical Conductivity: Equal Weight (Specific), % IACS 110
65

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 3.0
3.2
Embodied Carbon, kg CO2/kg material 8.0
8.7
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1140
1100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 25
2.2
Resilience: Unit (Modulus of Resilience), kJ/m3 350 to 430
280
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 46
43
Strength to Weight: Axial, points 25 to 31
20
Strength to Weight: Bending, points 31 to 36
26
Thermal Diffusivity, mm2/s 58
35
Thermal Shock Resistance, points 11 to 14
11

Alloy Composition


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Aluminum (Al), % 91.2 to 93.2
81.7 to 86.9
Chromium (Cr), % 0.060 to 0.2
0
Copper (Cu), % 0 to 0.1
7.0 to 9.0
Iron (Fe), % 0 to 0.15
0 to 0.5
Magnesium (Mg), % 0.6 to 0.8
5.5 to 6.5
Manganese (Mn), % 0 to 0.1
0.3 to 0.7
Nickel (Ni), % 0
0.3 to 0.7
Silicon (Si), % 0 to 0.15
0 to 0.5
Titanium (Ti), % 0.1 to 0.2
0 to 0.2
Zinc (Zn), % 6.0 to 7.0
0 to 0.1
Residuals, % 0 to 0.15
0 to 0.15