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ASTM A387 Grade 12 Steel vs. 713.0 Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
35
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
3.1
Embodied Carbon, kg CO2/kg material 1.6
7.8
Embodied Energy, MJ/kg 21
150
Embodied Water, L/kg 51
1110

Common Calculations

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

Alloy Composition

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