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380.0 Aluminum vs. SAE-AISI 1527 Steel

380.0 aluminum belongs to the aluminum alloys classification, while SAE-AISI 1527 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 380.0 aluminum and the bottom bar is SAE-AISI 1527 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
170 to 180
Elastic (Young's, Tensile) Modulus, GPa 74
190
Elongation at Break, % 3.0
13 to 21
Fatigue Strength, MPa 140
220 to 350
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 28
73
Shear Strength, MPa 190
370 to 390
Tensile Strength: Ultimate (UTS), MPa 320
590 to 640
Tensile Strength: Yield (Proof), MPa 160
320 to 550

Thermal Properties

Latent Heat of Fusion, J/g 510
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 590
1460
Melting Onset (Solidus), °C 540
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 100
52
Thermal Expansion, µm/m-K 22
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
7.1
Electrical Conductivity: Equal Weight (Specific), % IACS 83
8.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
1.8
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 7.5
1.4
Embodied Energy, MJ/kg 140
19
Embodied Water, L/kg 1040
47

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.0
82 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 170
260 to 800
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 48
24
Strength to Weight: Axial, points 31
21 to 23
Strength to Weight: Bending, points 36
20 to 21
Thermal Diffusivity, mm2/s 40
14
Thermal Shock Resistance, points 14
19 to 20

Alloy Composition

Aluminum (Al), % 79.6 to 89.5
0
Carbon (C), % 0
0.22 to 0.29
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 2.0
98.1 to 98.6
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
1.2 to 1.5
Nickel (Ni), % 0 to 0.5
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 7.5 to 9.5
0
Sulfur (S), % 0
0 to 0.050
Tin (Sn), % 0 to 0.35
0
Zinc (Zn), % 0 to 3.0
0
Residuals, % 0 to 0.5
0