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4032 Aluminum vs. SAE-AISI 1035 Steel

4032 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1035 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 4032 aluminum and the bottom bar is SAE-AISI 1035 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 120
160 to 180
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 6.7
13 to 21
Fatigue Strength, MPa 110
210 to 340
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
73
Shear Strength, MPa 260
360 to 370
Tensile Strength: Ultimate (UTS), MPa 390
570 to 620
Tensile Strength: Yield (Proof), MPa 320
300 to 530

Thermal Properties

Latent Heat of Fusion, J/g 570
250
Maximum Temperature: Mechanical, °C 180
400
Melting Completion (Liquidus), °C 570
1460
Melting Onset (Solidus), °C 530
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
51
Thermal Expansion, µm/m-K 19
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
7.0
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.0

Otherwise Unclassified Properties

Base Metal Price, % relative 10
1.8
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 7.8
1.4
Embodied Energy, MJ/kg 140
18
Embodied Water, L/kg 1030
46

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25
79 to 99
Resilience: Unit (Modulus of Resilience), kJ/m3 700
250 to 740
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 53
24
Strength to Weight: Axial, points 41
20 to 22
Strength to Weight: Bending, points 45
19 to 21
Thermal Diffusivity, mm2/s 59
14
Thermal Shock Resistance, points 20
18 to 20

Alloy Composition

Aluminum (Al), % 81.1 to 87.2
0
Carbon (C), % 0
0.32 to 0.38
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0.5 to 1.3
0
Iron (Fe), % 0 to 1.0
98.6 to 99.08
Magnesium (Mg), % 0.8 to 1.3
0
Manganese (Mn), % 0
0.6 to 0.9
Nickel (Ni), % 0.5 to 1.3
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 11 to 13.5
0
Sulfur (S), % 0
0 to 0.050
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0