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710.0 Aluminum vs. AISI 316N Stainless Steel

710.0 aluminum belongs to the aluminum alloys classification, while AISI 316N stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (3, 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 710.0 aluminum and the bottom bar is AISI 316N stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75
190 to 350
Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 3.6
9.0 to 39
Fatigue Strength, MPa 55 to 110
230 to 450
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
78
Shear Strength, MPa 180
420 to 690
Tensile Strength: Ultimate (UTS), MPa 240 to 250
620 to 1160
Tensile Strength: Yield (Proof), MPa 160
270 to 870

Thermal Properties

Latent Heat of Fusion, J/g 380
290
Maximum Temperature: Mechanical, °C 170
940
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 610
1400
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140
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 1130
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.9 to 7.9
95 to 230
Resilience: Unit (Modulus of Resilience), kJ/m3 180 to 190
180 to 1880
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 23
22 to 41
Strength to Weight: Bending, points 29
20 to 31
Thermal Diffusivity, mm2/s 53
4.1
Thermal Shock Resistance, points 10 to 11
14 to 26

Alloy Composition

Aluminum (Al), % 90.5 to 93.1
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0.35 to 0.65
0
Iron (Fe), % 0 to 0.5
61.9 to 71.9
Magnesium (Mg), % 0.6 to 0.8
0
Manganese (Mn), % 0 to 0.050
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 to 0.25
0
Zinc (Zn), % 6.0 to 7.0
0
Residuals, % 0 to 0.15
0