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512.0 Aluminum vs. SAE-AISI 4028 Steel

512.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4028 steel belongs to the iron 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 512.0 aluminum and the bottom bar is SAE-AISI 4028 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 50
150 to 190
Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 2.0
14 to 23
Fatigue Strength, MPa 58
180 to 330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 130
490 to 630
Tensile Strength: Yield (Proof), MPa 83
260 to 520

Thermal Properties

Latent Heat of Fusion, J/g 420
250
Maximum Temperature: Mechanical, °C 180
400
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 590
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
49
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
7.1
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.1
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.8
1.5
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1160
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3
81 to 95
Resilience: Unit (Modulus of Resilience), kJ/m3 50
180 to 720
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 14
17 to 22
Strength to Weight: Bending, points 22
18 to 21
Thermal Diffusivity, mm2/s 60
13
Thermal Shock Resistance, points 6.1
16 to 20

Alloy Composition

Aluminum (Al), % 90.6 to 95.1
0
Carbon (C), % 0
0.25 to 0.3
Chromium (Cr), % 0 to 0.25
0
Copper (Cu), % 0 to 0.35
0
Iron (Fe), % 0 to 0.6
98.1 to 98.7
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0 to 0.8
0.7 to 0.9
Molybdenum (Mo), % 0
0.2 to 0.3
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 1.4 to 2.2
0.15 to 0.35
Sulfur (S), % 0
0.035 to 0.050
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0