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ASTM A372 Grade M Steel vs. 5083 Aluminum

ASTM A372 grade M steel belongs to the iron alloys classification, while 5083 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 M steel and the bottom bar is 5083 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 240 to 280
75 to 110
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 18 to 21
1.1 to 17
Fatigue Strength, MPa 450 to 520
93 to 190
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
26
Shear Strength, MPa 510 to 570
170 to 220
Tensile Strength: Ultimate (UTS), MPa 810 to 910
290 to 390
Tensile Strength: Yield (Proof), MPa 660 to 770
110 to 340

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 450
190
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
580
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 46
120
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.0
29
Electrical Conductivity: Equal Weight (Specific), % IACS 9.1
96

Otherwise Unclassified Properties

Base Metal Price, % relative 5.0
9.5
Density, g/cm3 7.9
2.7
Embodied Carbon, kg CO2/kg material 2.0
8.9
Embodied Energy, MJ/kg 27
150
Embodied Water, L/kg 61
1170

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 160
4.2 to 42
Resilience: Unit (Modulus of Resilience), kJ/m3 1140 to 1580
95 to 860
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 29 to 32
29 to 40
Strength to Weight: Bending, points 24 to 27
36 to 44
Thermal Diffusivity, mm2/s 12
48
Thermal Shock Resistance, points 24 to 27
12 to 17

Alloy Composition

Aluminum (Al), % 0
92.4 to 95.6
Carbon (C), % 0 to 0.23
0
Chromium (Cr), % 1.5 to 2.0
0.050 to 0.25
Copper (Cu), % 0
0 to 0.1
Iron (Fe), % 92.5 to 95.1
0 to 0.4
Magnesium (Mg), % 0
4.0 to 4.9
Manganese (Mn), % 0.2 to 0.4
0.4 to 1.0
Molybdenum (Mo), % 0.4 to 0.6
0
Nickel (Ni), % 2.8 to 3.9
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.3
0 to 0.4
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0
0 to 0.15
Vanadium (V), % 0 to 0.080
0
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants