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4032 Aluminum vs. EN 1.7335 Steel

4032 aluminum belongs to the aluminum alloys classification, while EN 1.7335 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 4032 aluminum and the bottom bar is EN 1.7335 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
150 to 160
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 6.7
21 to 22
Fatigue Strength, MPa 110
200 to 220
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
73
Shear Strength, MPa 260
310 to 330
Tensile Strength: Ultimate (UTS), MPa 390
500 to 520
Tensile Strength: Yield (Proof), MPa 320
280 to 310

Thermal Properties

Latent Heat of Fusion, J/g 570
250
Maximum Temperature: Mechanical, °C 180
430
Melting Completion (Liquidus), °C 570
1470
Melting Onset (Solidus), °C 530
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
44
Thermal Expansion, µm/m-K 19
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
7.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
2.8
Density, g/cm3 2.6
7.9
Embodied Carbon, kg CO2/kg material 7.8
1.6
Embodied Energy, MJ/kg 140
21
Embodied Water, L/kg 1030
52

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25
91 to 97
Resilience: Unit (Modulus of Resilience), kJ/m3 700
210 to 260
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 53
24
Strength to Weight: Axial, points 41
18
Strength to Weight: Bending, points 45
18
Thermal Diffusivity, mm2/s 59
12
Thermal Shock Resistance, points 20
15

Alloy Composition

Aluminum (Al), % 81.1 to 87.2
0
Carbon (C), % 0
0.080 to 0.18
Chromium (Cr), % 0 to 0.1
0.7 to 1.2
Copper (Cu), % 0.5 to 1.3
0 to 0.3
Iron (Fe), % 0 to 1.0
96.4 to 98.4
Magnesium (Mg), % 0.8 to 1.3
0
Manganese (Mn), % 0
0.4 to 1.0
Molybdenum (Mo), % 0
0.4 to 0.6
Nickel (Ni), % 0.5 to 1.3
0
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 11 to 13.5
0 to 0.35
Sulfur (S), % 0
0 to 0.010
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0