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7050 Aluminum vs. EN 1.8519 Steel

7050 aluminum belongs to the aluminum alloys classification, while EN 1.8519 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 7050 aluminum and the bottom bar is EN 1.8519 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 2.2 to 12
10
Fatigue Strength, MPa 130 to 210
630
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 280 to 330
710
Tensile Strength: Ultimate (UTS), MPa 490 to 570
1200
Tensile Strength: Yield (Proof), MPa 390 to 500
1030

Thermal Properties

Latent Heat of Fusion, J/g 370
250
Maximum Temperature: Mechanical, °C 190
450
Melting Completion (Liquidus), °C 630
1460
Melting Onset (Solidus), °C 490
1420
Specific Heat Capacity, J/kg-K 860
470
Thermal Conductivity, W/m-K 140
40
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.1
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1120
58

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
120
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
2790
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 45 to 51
43
Strength to Weight: Bending, points 45 to 50
32
Thermal Diffusivity, mm2/s 54
11
Thermal Shock Resistance, points 21 to 25
35

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0.27 to 0.34
Chromium (Cr), % 0 to 0.040
2.3 to 2.7
Copper (Cu), % 2.0 to 2.6
0
Iron (Fe), % 0 to 0.15
95.7 to 97.1
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0.4 to 0.7
Molybdenum (Mo), % 0
0.15 to 0.25
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.12
0 to 0.4
Sulfur (S), % 0
0 to 0.035
Titanium (Ti), % 0 to 0.060
0
Vanadium (V), % 0
0.1 to 0.2
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0