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5154A Aluminum vs. 511.0 Aluminum

Both 5154A aluminum and 511.0 aluminum are aluminum alloys. Their average alloy composition is basically identical.

For each property being compared, the top bar is 5154A aluminum and the bottom bar is 511.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 58 to 100
50
Elastic (Young's, Tensile) Modulus, GPa 68
68
Elongation at Break, % 1.1 to 19
3.0
Fatigue Strength, MPa 83 to 160
55
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
25
Shear Strength, MPa 140 to 210
120
Tensile Strength: Ultimate (UTS), MPa 230 to 370
150
Tensile Strength: Yield (Proof), MPa 96 to 320
83

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 190
170
Melting Completion (Liquidus), °C 650
640
Melting Onset (Solidus), °C 600
590
Specific Heat Capacity, J/kg-K 900
900
Thermal Conductivity, W/m-K 130
140
Thermal Expansion, µm/m-K 24
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
36
Electrical Conductivity: Equal Weight (Specific), % IACS 110
120

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
2.7
Embodied Carbon, kg CO2/kg material 8.8
8.8
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1180
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 36
3.7
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 760
51
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
51
Strength to Weight: Axial, points 24 to 38
15
Strength to Weight: Bending, points 31 to 43
23
Thermal Diffusivity, mm2/s 53
59
Thermal Shock Resistance, points 10 to 16
6.5

Alloy Composition

Aluminum (Al), % 93.7 to 96.9
93.3 to 96.2
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.1
0 to 0.15
Iron (Fe), % 0 to 0.5
0 to 0.5
Magnesium (Mg), % 3.1 to 3.9
3.5 to 4.5
Manganese (Mn), % 0 to 0.5
0 to 0.35
Silicon (Si), % 0 to 0.5
0.3 to 0.7
Titanium (Ti), % 0 to 0.2
0 to 0.25
Zinc (Zn), % 0 to 0.2
0 to 0.15
Residuals, % 0
0 to 0.15