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1100-H18 Aluminum vs. 5056-H18 Aluminum

Both 1100-H18 aluminum and 5056-H18 aluminum are aluminum alloys. Both are furnished in the H18 temper. They have a moderately high 95% of their average alloy composition in common.

For each property being compared, the top bar is 1100-H18 aluminum and the bottom bar is 5056-H18 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 44
110
Elastic (Young's, Tensile) Modulus, GPa 69
67
Elongation at Break, % 5.5
9.7
Fatigue Strength, MPa 61
150
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
25
Shear Strength, MPa 90
240
Tensile Strength: Ultimate (UTS), MPa 170
440
Tensile Strength: Yield (Proof), MPa 150
410

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 180
190
Melting Completion (Liquidus), °C 660
640
Melting Onset (Solidus), °C 640
570
Specific Heat Capacity, J/kg-K 900
910
Thermal Conductivity, W/m-K 220
130
Thermal Expansion, µm/m-K 24
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 59
29
Electrical Conductivity: Equal Weight (Specific), % IACS 190
99

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.5
Calomel Potential, mV -740
-780
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.2
9.0
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.0
41
Resilience: Unit (Modulus of Resilience), kJ/m3 170
1220
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
51
Strength to Weight: Axial, points 17
46
Strength to Weight: Bending, points 25
48
Thermal Diffusivity, mm2/s 90
53
Thermal Shock Resistance, points 7.4
19

Alloy Composition

Aluminum (Al), % 99 to 99.95
93 to 95.4
Chromium (Cr), % 0
0.050 to 0.2
Copper (Cu), % 0.050 to 0.2
0 to 0.1
Iron (Fe), % 0 to 1.0
0 to 0.4
Magnesium (Mg), % 0
4.5 to 5.6
Manganese (Mn), % 0 to 0.050
0.050 to 0.2
Silicon (Si), % 0 to 1.0
0 to 0.3
Zinc (Zn), % 0 to 0.1
0 to 0.1
Residuals, % 0
0 to 0.15