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2011 Aluminum vs. EN 1.4913 Stainless Steel

2011 aluminum belongs to the aluminum alloys classification, while EN 1.4913 stainless steel belongs to the iron 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 2011 aluminum and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 8.5 to 18
14 to 22
Fatigue Strength, MPa 74 to 120
320 to 480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
75
Shear Strength, MPa 190 to 250
550 to 590
Tensile Strength: Ultimate (UTS), MPa 310 to 420
870 to 980
Tensile Strength: Yield (Proof), MPa 140 to 310
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 190
700
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 140 to 170
24
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35 to 45
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100 to 130
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.0
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 7.9
2.9
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1150
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 29 to 52
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 680
600 to 1860
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 44
25
Strength to Weight: Axial, points 27 to 37
31 to 35
Strength to Weight: Bending, points 32 to 40
26 to 28
Thermal Diffusivity, mm2/s 51 to 64
6.5
Thermal Shock Resistance, points 14 to 19
31 to 34

Alloy Composition

Aluminum (Al), % 91.3 to 94.6
0 to 0.020
Bismuth (Bi), % 0.2 to 0.6
0
Boron (B), % 0
0 to 0.0015
Carbon (C), % 0
0.17 to 0.23
Chromium (Cr), % 0
10 to 11.5
Copper (Cu), % 5.0 to 6.0
0
Iron (Fe), % 0 to 0.7
84.5 to 88.3
Lead (Pb), % 0.2 to 0.6
0
Manganese (Mn), % 0
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0
0.2 to 0.6
Niobium (Nb), % 0
0.25 to 0.55
Nitrogen (N), % 0
0.050 to 0.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.4
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Vanadium (V), % 0
0.1 to 0.3
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.15
0