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EN AC-41000 Aluminum vs. N08800 Stainless Steel

EN AC-41000 aluminum belongs to the aluminum alloys classification, while N08800 stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 AC-41000 aluminum and the bottom bar is N08800 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 4.5
4.5 to 34
Fatigue Strength, MPa 58 to 71
150 to 390
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Tensile Strength: Ultimate (UTS), MPa 170 to 280
500 to 1000
Tensile Strength: Yield (Proof), MPa 80 to 210
190 to 830

Thermal Properties

Latent Heat of Fusion, J/g 420
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 640
1390
Melting Onset (Solidus), °C 630
1360
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 170
12
Thermal Expansion, µm/m-K 23
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 130
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
30
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 8.2
5.3
Embodied Energy, MJ/kg 150
76
Embodied Water, L/kg 1160
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.4 to 11
42 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 46 to 300
96 to 1740
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 18 to 29
18 to 35
Strength to Weight: Bending, points 26 to 35
18 to 28
Thermal Diffusivity, mm2/s 69
3.0
Thermal Shock Resistance, points 7.8 to 13
13 to 25

Alloy Composition

Aluminum (Al), % 95.2 to 97.6
0.15 to 0.6
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0
19 to 23
Copper (Cu), % 0 to 0.1
0 to 0.75
Iron (Fe), % 0 to 0.6
39.5 to 50.7
Lead (Pb), % 0 to 0.050
0
Magnesium (Mg), % 0.45 to 0.65
0
Manganese (Mn), % 0.3 to 0.5
0 to 1.5
Nickel (Ni), % 0 to 0.050
30 to 35
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 1.6 to 2.4
0 to 1.0
Sulfur (S), % 0
0 to 0.015
Tin (Sn), % 0 to 0.050
0
Titanium (Ti), % 0.050 to 0.2
0.15 to 0.6
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0