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772.0 Aluminum vs. AISI 316N Stainless Steel

772.0 aluminum belongs to the aluminum alloys classification, while AISI 316N stainless steel belongs to the iron alloys. There are 29 material properties with values for both materials. Properties with values for just one material (4, 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 772.0 aluminum and the bottom bar is AISI 316N stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
200
Elongation at Break, % 6.3 to 8.4
9.0 to 39
Fatigue Strength, MPa 94 to 160
230 to 450
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
78
Tensile Strength: Ultimate (UTS), MPa 260 to 320
620 to 1160
Tensile Strength: Yield (Proof), MPa 220 to 250
270 to 870

Thermal Properties

Latent Heat of Fusion, J/g 380
290
Maximum Temperature: Mechanical, °C 180
940
Melting Completion (Liquidus), °C 630
1440
Melting Onset (Solidus), °C 580
1400
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 150
15
Thermal Expansion, µm/m-K 24
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 3.0
7.9
Embodied Carbon, kg CO2/kg material 8.0
3.9
Embodied Energy, MJ/kg 150
53
Embodied Water, L/kg 1140
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 16 to 25
95 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 350 to 430
180 to 1880
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 25 to 31
22 to 41
Strength to Weight: Bending, points 31 to 36
20 to 31
Thermal Diffusivity, mm2/s 58
4.1
Thermal Shock Resistance, points 11 to 14
14 to 26

Alloy Composition

Aluminum (Al), % 91.2 to 93.2
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0.060 to 0.2
16 to 18
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 0.15
61.9 to 71.9
Magnesium (Mg), % 0.6 to 0.8
0
Manganese (Mn), % 0 to 0.1
0 to 2.0
Molybdenum (Mo), % 0
2.0 to 3.0
Nickel (Ni), % 0
10 to 14
Nitrogen (N), % 0
0.1 to 0.16
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.15
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0.1 to 0.2
0
Zinc (Zn), % 6.0 to 7.0
0
Residuals, % 0 to 0.15
0