MakeItFrom.com
Menu (ESC)

332.0 Aluminum vs. EN 1.7380 Steel

332.0 aluminum belongs to the aluminum alloys classification, while EN 1.7380 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 332.0 aluminum and the bottom bar is EN 1.7380 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 110
160 to 170
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 1.0
19 to 20
Fatigue Strength, MPa 90
200 to 230
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 190
330 to 350
Tensile Strength: Ultimate (UTS), MPa 250
540 to 550
Tensile Strength: Yield (Proof), MPa 190
290 to 330

Thermal Properties

Latent Heat of Fusion, J/g 530
260
Maximum Temperature: Mechanical, °C 170
460
Melting Completion (Liquidus), °C 580
1470
Melting Onset (Solidus), °C 530
1430
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 100
39
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 26
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 84
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.8
Density, g/cm3 2.8
7.9
Embodied Carbon, kg CO2/kg material 7.8
1.8
Embodied Energy, MJ/kg 140
23
Embodied Water, L/kg 1040
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3
87 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 250
230 to 280
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 24
19 to 20
Strength to Weight: Bending, points 31
19
Thermal Diffusivity, mm2/s 42
11
Thermal Shock Resistance, points 12
15 to 16

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
Aluminum (Al), % 80.1 to 89
0
Carbon (C), % 0
0.080 to 0.14
Chromium (Cr), % 0
2.0 to 2.5
Copper (Cu), % 2.0 to 4.0
0 to 0.3
Iron (Fe), % 0 to 1.2
94.6 to 96.6
Magnesium (Mg), % 0.5 to 1.5
0
Manganese (Mn), % 0 to 0.5
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0 to 0.5
0
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 8.5 to 10.5
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0