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ASTM A372 Grade J Steel vs. 512.0 Aluminum

ASTM A372 grade J steel belongs to the iron alloys classification, while 512.0 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 A372 grade J steel and the bottom bar is 512.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 200 to 310
50
Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 17 to 22
2.0
Fatigue Strength, MPa 310 to 570
58
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Tensile Strength: Ultimate (UTS), MPa 650 to 1020
130
Tensile Strength: Yield (Proof), MPa 430 to 850
83

Thermal Properties

Latent Heat of Fusion, J/g 250
420
Maximum Temperature: Mechanical, °C 420
180
Melting Completion (Liquidus), °C 1460
630
Melting Onset (Solidus), °C 1420
590
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 44
150
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.3
38
Electrical Conductivity: Equal Weight (Specific), % IACS 8.4
130

Otherwise Unclassified Properties

Base Metal Price, % relative 2.4
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.5
8.8
Embodied Energy, MJ/kg 20
150
Embodied Water, L/kg 51
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130 to 170
2.3
Resilience: Unit (Modulus of Resilience), kJ/m3 500 to 1930
50
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 23 to 36
14
Strength to Weight: Bending, points 21 to 29
22
Thermal Diffusivity, mm2/s 12
60
Thermal Shock Resistance, points 19 to 30
6.1

Alloy Composition


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Aluminum (Al), % 0
90.6 to 95.1
Carbon (C), % 0.35 to 0.5
0
Chromium (Cr), % 0.8 to 1.2
0 to 0.25
Copper (Cu), % 0
0 to 0.35
Iron (Fe), % 96.7 to 97.8
0 to 0.6
Magnesium (Mg), % 0
3.5 to 4.5
Manganese (Mn), % 0.75 to 1.1
0 to 0.8
Molybdenum (Mo), % 0.15 to 0.25
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0.15 to 0.35
1.4 to 2.2
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15