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384.0 Aluminum vs. ASTM A387 Grade 21 Steel

384.0 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 21 steel belongs to the iron 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 384.0 aluminum and the bottom bar is ASTM A387 grade 21 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85
150 to 180
Elastic (Young's, Tensile) Modulus, GPa 74
190
Elongation at Break, % 2.5
21
Fatigue Strength, MPa 140
160 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
74
Shear Strength, MPa 200
310 to 370
Tensile Strength: Ultimate (UTS), MPa 330
500 to 590
Tensile Strength: Yield (Proof), MPa 170
230 to 350

Thermal Properties

Latent Heat of Fusion, J/g 550
260
Maximum Temperature: Mechanical, °C 170
480
Melting Completion (Liquidus), °C 580
1470
Melting Onset (Solidus), °C 530
1430
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 96
41
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 22
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 69
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 11
4.1
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 7.4
1.8
Embodied Energy, MJ/kg 140
23
Embodied Water, L/kg 1010
62

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.9
84 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 190
140 to 320
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 32
18 to 21
Strength to Weight: Bending, points 37
18 to 20
Thermal Diffusivity, mm2/s 39
11
Thermal Shock Resistance, points 15
14 to 17

Alloy Composition

Aluminum (Al), % 77.3 to 86.5
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0
2.8 to 3.3
Copper (Cu), % 3.0 to 4.5
0
Iron (Fe), % 0 to 1.3
94.4 to 96
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.5
0
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 10.5 to 12
0 to 0.5
Sulfur (S), % 0
0 to 0.025
Tin (Sn), % 0 to 0.35
0
Zinc (Zn), % 0 to 3.0
0
Residuals, % 0 to 0.5
0