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ASTM A387 Grade 12 Steel vs. EN AC-51300 Aluminum

ASTM A387 grade 12 steel belongs to the iron alloys classification, while EN AC-51300 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (2, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is ASTM A387 grade 12 steel and the bottom bar is EN AC-51300 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140 to 160
65
Elastic (Young's, Tensile) Modulus, GPa 190
67
Elongation at Break, % 25
3.7
Fatigue Strength, MPa 190 to 230
78
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
25
Tensile Strength: Ultimate (UTS), MPa 470 to 520
190
Tensile Strength: Yield (Proof), MPa 260 to 310
110

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 430
170
Melting Completion (Liquidus), °C 1470
640
Melting Onset (Solidus), °C 1420
600
Specific Heat Capacity, J/kg-K 470
910
Thermal Conductivity, W/m-K 44
110
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
31
Electrical Conductivity: Equal Weight (Specific), % IACS 8.3
100

Otherwise Unclassified Properties

Base Metal Price, % relative 2.8
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.6
9.1
Embodied Energy, MJ/kg 21
150
Embodied Water, L/kg 51
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 110
6.1
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 250
87
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 16 to 18
20
Strength to Weight: Bending, points 17 to 18
28
Thermal Diffusivity, mm2/s 12
45
Thermal Shock Resistance, points 14 to 15
8.6

Alloy Composition

Aluminum (Al), % 0
91.4 to 95.5
Carbon (C), % 0.050 to 0.17
0
Chromium (Cr), % 0.8 to 1.2
0
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 97 to 98.2
0 to 0.55
Magnesium (Mg), % 0
4.5 to 6.5
Manganese (Mn), % 0.4 to 0.65
0 to 0.45
Molybdenum (Mo), % 0.45 to 0.6
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.15 to 0.4
0 to 0.55
Sulfur (S), % 0 to 0.025
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15