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EN AC-44500 Aluminum vs. AISI 316 Stainless Steel

EN AC-44500 aluminum belongs to the aluminum alloys classification, while AISI 316 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (6, 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-44500 aluminum and the bottom bar is AISI 316 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 68
160 to 360
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 1.1
8.0 to 55
Fatigue Strength, MPa 110
210 to 430
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Tensile Strength: Ultimate (UTS), MPa 270
520 to 1180
Tensile Strength: Yield (Proof), MPa 160
230 to 850

Thermal Properties

Latent Heat of Fusion, J/g 570
290
Maximum Temperature: Mechanical, °C 170
590
Melting Completion (Liquidus), °C 590
1400
Melting Onset (Solidus), °C 580
1380
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 21
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
2.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 2.5
7.9
Embodied Carbon, kg CO2/kg material 7.7
3.9
Embodied Energy, MJ/kg 140
53
Embodied Water, L/kg 1050
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.6
85 to 260
Resilience: Unit (Modulus of Resilience), kJ/m3 180
130 to 1820
Stiffness to Weight: Axial, points 16
14
Stiffness to Weight: Bending, points 55
25
Strength to Weight: Axial, points 29
18 to 41
Strength to Weight: Bending, points 36
18 to 31
Thermal Diffusivity, mm2/s 57
4.1
Thermal Shock Resistance, points 13
11 to 26

Alloy Composition

Aluminum (Al), % 83.7 to 89.5
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 1.0
62 to 72
Magnesium (Mg), % 0 to 0.4
0
Manganese (Mn), % 0 to 0.55
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0
10 to 14
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 10.5 to 13.5
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.3
0
Residuals, % 0 to 0.25
0