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713.0 Aluminum vs. ASTM A387 Grade 12 Steel

713.0 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 12 steel belongs to the iron alloys. There are 31 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 713.0 aluminum and the bottom bar is ASTM A387 grade 12 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 74 to 75
140 to 160
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 3.9 to 4.3
25
Fatigue Strength, MPa 63 to 120
190 to 230
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 27
73
Shear Strength, MPa 180
300 to 330
Tensile Strength: Ultimate (UTS), MPa 240 to 260
470 to 520
Tensile Strength: Yield (Proof), MPa 170
260 to 310

Thermal Properties

Latent Heat of Fusion, J/g 370
250
Maximum Temperature: Mechanical, °C 180
430
Melting Completion (Liquidus), °C 630
1470
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 150
44
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.8
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 7.8
1.6
Embodied Energy, MJ/kg 150
21
Embodied Water, L/kg 1110
51

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.7 to 9.9
98 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 220
180 to 250
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 22 to 23
16 to 18
Strength to Weight: Bending, points 28 to 29
17 to 18
Thermal Diffusivity, mm2/s 57
12
Thermal Shock Resistance, points 10 to 11
14 to 15

Alloy Composition

Aluminum (Al), % 87.6 to 92.4
0
Carbon (C), % 0
0.050 to 0.17
Chromium (Cr), % 0 to 0.35
0.8 to 1.2
Copper (Cu), % 0.4 to 1.0
0
Iron (Fe), % 0 to 1.1
97 to 98.2
Magnesium (Mg), % 0.2 to 0.5
0
Manganese (Mn), % 0 to 0.6
0.4 to 0.65
Molybdenum (Mo), % 0
0.45 to 0.6
Nickel (Ni), % 0 to 0.15
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.25
0.15 to 0.4
Sulfur (S), % 0
0 to 0.025
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 7.0 to 8.0
0
Residuals, % 0 to 0.25
0