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EN 1.4935 Stainless Steel vs. 6014 Aluminum

EN 1.4935 stainless steel belongs to the iron alloys classification, while 6014 aluminum belongs to the aluminum alloys. There are 30 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 EN 1.4935 stainless steel and the bottom bar is 6014 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 16 to 18
9.1 to 17
Fatigue Strength, MPa 350 to 400
43 to 79
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Shear Strength, MPa 480 to 540
96 to 150
Tensile Strength: Ultimate (UTS), MPa 780 to 880
160 to 260
Tensile Strength: Yield (Proof), MPa 570 to 670
80 to 200

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Maximum Temperature: Mechanical, °C 740
180
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
620
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 24
200
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
53
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
180

Otherwise Unclassified Properties

Base Metal Price, % relative 9.0
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 2.9
8.6
Embodied Energy, MJ/kg 42
160
Embodied Water, L/kg 100
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
22
Resilience: Unit (Modulus of Resilience), kJ/m3 830 to 1160
46 to 300
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 28 to 31
16 to 26
Strength to Weight: Bending, points 24 to 26
24 to 33
Thermal Diffusivity, mm2/s 6.5
83
Thermal Shock Resistance, points 27 to 30
7.0 to 11

Alloy Composition

Aluminum (Al), % 0
97.1 to 99.2
Carbon (C), % 0.17 to 0.24
0
Chromium (Cr), % 11 to 12.5
0 to 0.2
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 83 to 86.7
0 to 0.35
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0.3 to 0.8
0.050 to 0.2
Molybdenum (Mo), % 0.8 to 1.2
0
Nickel (Ni), % 0.3 to 0.8
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0.1 to 0.5
0.3 to 0.6
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.1
Tungsten (W), % 0.4 to 0.6
0
Vanadium (V), % 0.2 to 0.35
0.050 to 0.2
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15

Comparable Variants