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413.0 Aluminum vs. EN 1.7767 Steel

413.0 aluminum belongs to the aluminum alloys classification, while EN 1.7767 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 413.0 aluminum and the bottom bar is EN 1.7767 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
200 to 210
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 2.5
20
Fatigue Strength, MPa 130
320 to 340
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
74
Shear Strength, MPa 170
420 to 430
Tensile Strength: Ultimate (UTS), MPa 270
670 to 690
Tensile Strength: Yield (Proof), MPa 140
460 to 500

Thermal Properties

Latent Heat of Fusion, J/g 570
250
Maximum Temperature: Mechanical, °C 170
480
Melting Completion (Liquidus), °C 590
1470
Melting Onset (Solidus), °C 580
1430
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
40
Thermal Expansion, µm/m-K 20
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.5
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.6
2.4
Embodied Energy, MJ/kg 140
33
Embodied Water, L/kg 1040
64

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.7
120 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 130
570 to 650
Stiffness to Weight: Axial, points 16
13
Stiffness to Weight: Bending, points 53
24
Strength to Weight: Axial, points 29
24
Strength to Weight: Bending, points 36
22
Thermal Diffusivity, mm2/s 59
11
Thermal Shock Resistance, points 13
19 to 20

Alloy Composition

Aluminum (Al), % 82.2 to 89
0
Carbon (C), % 0
0.1 to 0.15
Chromium (Cr), % 0
2.8 to 3.3
Copper (Cu), % 0 to 1.0
0 to 0.25
Iron (Fe), % 0 to 2.0
93.8 to 95.8
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.35
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.5
0 to 0.25
Niobium (Nb), % 0
0 to 0.070
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 11 to 13
0 to 0.15
Sulfur (S), % 0
0 to 0.0050
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0
0 to 0.030
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.25
0