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EN 1.1221 Steel vs. 296.0 Aluminum

EN 1.1221 steel belongs to the iron alloys classification, while 296.0 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 EN 1.1221 steel and the bottom bar is 296.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 250
75 to 90
Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 10 to 21
3.2 to 7.1
Fatigue Strength, MPa 240 to 340
47 to 70
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 72
27
Tensile Strength: Ultimate (UTS), MPa 730 to 870
260 to 270
Tensile Strength: Yield (Proof), MPa 390 to 550
120 to 180

Thermal Properties

Latent Heat of Fusion, J/g 250
420
Maximum Temperature: Mechanical, °C 400
170
Melting Completion (Liquidus), °C 1460
630
Melting Onset (Solidus), °C 1410
540
Specific Heat Capacity, J/kg-K 470
870
Thermal Conductivity, W/m-K 48
130 to 150
Thermal Expansion, µm/m-K 12
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.2
33 to 37
Electrical Conductivity: Equal Weight (Specific), % IACS 8.3
99 to 110

Otherwise Unclassified Properties

Base Metal Price, % relative 2.1
11
Density, g/cm3 7.8
3.0
Embodied Carbon, kg CO2/kg material 1.5
7.8
Embodied Energy, MJ/kg 19
150
Embodied Water, L/kg 47
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 67 to 130
7.6 to 15
Resilience: Unit (Modulus of Resilience), kJ/m3 410 to 800
110 to 220
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
46
Strength to Weight: Axial, points 26 to 31
24 to 25
Strength to Weight: Bending, points 23 to 26
30 to 31
Thermal Diffusivity, mm2/s 13
51 to 56
Thermal Shock Resistance, points 23 to 28
12

Alloy Composition

Aluminum (Al), % 0
89 to 94
Carbon (C), % 0.57 to 0.65
0
Chromium (Cr), % 0 to 0.4
0
Copper (Cu), % 0
4.0 to 5.0
Iron (Fe), % 97.1 to 98.8
0 to 1.2
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0.6 to 0.9
0 to 0.35
Molybdenum (Mo), % 0 to 0.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.35
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0 to 0.4
2.0 to 3.0
Sulfur (S), % 0 to 0.035
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.35