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EN AC-21100 Aluminum vs. EN 1.7362 Steel

EN AC-21100 aluminum belongs to the aluminum alloys classification, while EN 1.7362 steel belongs to the iron alloys. There are 30 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 EN AC-21100 aluminum and the bottom bar is EN 1.7362 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 110
150 to 180
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 6.2 to 7.3
21 to 22
Fatigue Strength, MPa 79 to 87
140 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Tensile Strength: Ultimate (UTS), MPa 340 to 350
510 to 600
Tensile Strength: Yield (Proof), MPa 210 to 240
200 to 360

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 170
510
Melting Completion (Liquidus), °C 670
1460
Melting Onset (Solidus), °C 550
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
8.1
Electrical Conductivity: Equal Weight (Specific), % IACS 100
9.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
4.5
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 8.0
1.8
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1150
69

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 21
90 to 110
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 400
100 to 340
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 31 to 33
18 to 21
Strength to Weight: Bending, points 36 to 37
18 to 20
Thermal Diffusivity, mm2/s 48
11
Thermal Shock Resistance, points 15
14 to 17

Alloy Composition

Aluminum (Al), % 93.4 to 95.7
0
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0
4.0 to 6.0
Copper (Cu), % 4.2 to 5.2
0 to 0.3
Iron (Fe), % 0 to 0.19
91.5 to 95.2
Manganese (Mn), % 0 to 0.55
0.3 to 0.6
Molybdenum (Mo), % 0
0.45 to 0.65
Nickel (Ni), % 0
0 to 0.3
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.18
0 to 0.5
Sulfur (S), % 0
0 to 0.0050
Titanium (Ti), % 0.15 to 0.3
0
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.1
0