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ASTM A387 Grade 2 Steel vs. 413.0 Aluminum

ASTM A387 grade 2 steel belongs to the iron alloys classification, while 413.0 aluminum belongs to the aluminum alloys. There are 31 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 A387 grade 2 steel and the bottom bar is 413.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 140 to 170
80
Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 25
2.5
Fatigue Strength, MPa 190 to 250
130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
28
Shear Strength, MPa 300 to 350
170
Tensile Strength: Ultimate (UTS), MPa 470 to 550
270
Tensile Strength: Yield (Proof), MPa 260 to 350
140

Thermal Properties

Latent Heat of Fusion, J/g 250
570
Maximum Temperature: Mechanical, °C 420
170
Melting Completion (Liquidus), °C 1470
590
Melting Onset (Solidus), °C 1420
580
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 45
140
Thermal Expansion, µm/m-K 13
20

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
35
Electrical Conductivity: Equal Weight (Specific), % IACS 8.3
120

Otherwise Unclassified Properties

Base Metal Price, % relative 2.6
9.5
Density, g/cm3 7.9
2.6
Embodied Carbon, kg CO2/kg material 1.6
7.6
Embodied Energy, MJ/kg 20
140
Embodied Water, L/kg 50
1040

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 98 to 120
5.7
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 320
130
Stiffness to Weight: Axial, points 13
16
Stiffness to Weight: Bending, points 24
53
Strength to Weight: Axial, points 16 to 20
29
Strength to Weight: Bending, points 17 to 19
36
Thermal Diffusivity, mm2/s 12
59
Thermal Shock Resistance, points 14 to 16
13

Alloy Composition

Aluminum (Al), % 0
82.2 to 89
Carbon (C), % 0.050 to 0.21
0
Chromium (Cr), % 0.5 to 0.8
0
Copper (Cu), % 0
0 to 1.0
Iron (Fe), % 97.1 to 98.3
0 to 2.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0.55 to 0.8
0 to 0.35
Molybdenum (Mo), % 0.45 to 0.6
0
Nickel (Ni), % 0
0 to 0.5
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.15 to 0.4
11 to 13
Sulfur (S), % 0 to 0.025
0
Tin (Sn), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.25