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7005 Aluminum vs. EN 1.6368 Steel

7005 aluminum belongs to the aluminum alloys classification, while EN 1.6368 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 7005 aluminum and the bottom bar is EN 1.6368 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 10 to 20
18
Fatigue Strength, MPa 100 to 190
310 to 330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 120 to 230
410 to 430
Tensile Strength: Ultimate (UTS), MPa 200 to 400
660 to 690
Tensile Strength: Yield (Proof), MPa 95 to 350
460 to 490

Thermal Properties

Latent Heat of Fusion, J/g 380
250
Maximum Temperature: Mechanical, °C 200
410
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 610
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 140 to 170
40
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 43
7.5
Electrical Conductivity: Equal Weight (Specific), % IACS 110 to 130
8.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.4
Density, g/cm3 2.9
7.9
Embodied Carbon, kg CO2/kg material 8.3
1.7
Embodied Energy, MJ/kg 150
22
Embodied Water, L/kg 1150
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 32 to 57
110
Resilience: Unit (Modulus of Resilience), kJ/m3 65 to 850
580 to 650
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 19 to 38
23 to 24
Strength to Weight: Bending, points 26 to 41
21 to 22
Thermal Diffusivity, mm2/s 54 to 65
11
Thermal Shock Resistance, points 8.7 to 18
20

Alloy Composition

Aluminum (Al), % 91 to 94.7
0.015 to 0.040
Carbon (C), % 0
0 to 0.17
Chromium (Cr), % 0.060 to 0.2
0 to 0.3
Copper (Cu), % 0 to 0.1
0.5 to 0.8
Iron (Fe), % 0 to 0.4
95.1 to 97.2
Magnesium (Mg), % 1.0 to 1.8
0
Manganese (Mn), % 0.2 to 0.7
0.8 to 1.2
Molybdenum (Mo), % 0
0.25 to 0.5
Nickel (Ni), % 0
1.0 to 1.3
Niobium (Nb), % 0
0.015 to 0.045
Nitrogen (N), % 0
0 to 0.020
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.35
0.25 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.010 to 0.060
0
Zinc (Zn), % 4.0 to 5.0
0
Zirconium (Zr), % 0.080 to 0.2
0
Residuals, % 0 to 0.15
0