MakeItFrom.com
Menu (ESC)

7108A Aluminum vs. EN 1.7383 Steel

7108A aluminum belongs to the aluminum alloys classification, while EN 1.7383 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 7108A aluminum and the bottom bar is EN 1.7383 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 11 to 13
20 to 23
Fatigue Strength, MPa 120 to 130
210 to 270
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 210
350 to 380
Tensile Strength: Ultimate (UTS), MPa 350
560 to 610
Tensile Strength: Yield (Proof), MPa 290 to 300
300 to 400

Thermal Properties

Latent Heat of Fusion, J/g 380
260
Maximum Temperature: Mechanical, °C 210
460
Melting Completion (Liquidus), °C 630
1470
Melting Onset (Solidus), °C 520
1430
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 150
39
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
7.7
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.9
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.8
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1150
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 38 to 44
110
Resilience: Unit (Modulus of Resilience), kJ/m3 610 to 640
240 to 420
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 33 to 34
20 to 22
Strength to Weight: Bending, points 38
19 to 20
Thermal Diffusivity, mm2/s 59
11
Thermal Shock Resistance, points 15 to 16
16 to 18

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 452
Aluminum (Al), % 91.6 to 94.4
0 to 0.040
Carbon (C), % 0
0.080 to 0.15
Chromium (Cr), % 0 to 0.040
2.0 to 2.5
Copper (Cu), % 0 to 0.050
0 to 0.3
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.3
94.3 to 96.6
Magnesium (Mg), % 0.7 to 1.5
0
Manganese (Mn), % 0 to 0.050
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.2
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.030
0
Zinc (Zn), % 4.8 to 5.8
0
Zirconium (Zr), % 0.15 to 0.25
0
Residuals, % 0 to 0.15
0