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EN AC-51200 Aluminum vs. AISI 347 Stainless Steel

EN AC-51200 aluminum belongs to the aluminum alloys classification, while AISI 347 stainless steel belongs to the iron alloys. There are 30 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 EN AC-51200 aluminum and the bottom bar is AISI 347 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 80
160 to 210
Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 1.1
34 to 46
Fatigue Strength, MPa 100
220 to 270
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
77
Tensile Strength: Ultimate (UTS), MPa 220
610 to 690
Tensile Strength: Yield (Proof), MPa 150
240 to 350

Thermal Properties

Latent Heat of Fusion, J/g 410
290
Maximum Temperature: Mechanical, °C 170
870
Melting Completion (Liquidus), °C 640
1430
Melting Onset (Solidus), °C 570
1400
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 92
16
Thermal Expansion, µm/m-K 23
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 22
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 74
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
19
Density, g/cm3 2.6
7.8
Embodied Carbon, kg CO2/kg material 9.6
3.6
Embodied Energy, MJ/kg 150
52
Embodied Water, L/kg 1150
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.2
190 to 220
Resilience: Unit (Modulus of Resilience), kJ/m3 160
150 to 310
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 24
22 to 25
Strength to Weight: Bending, points 31
20 to 22
Thermal Diffusivity, mm2/s 39
4.3
Thermal Shock Resistance, points 10
13 to 15

Alloy Composition

Aluminum (Al), % 84.5 to 92
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
17 to 19
Copper (Cu), % 0 to 0.1
0
Iron (Fe), % 0 to 1.0
64.1 to 74
Lead (Pb), % 0 to 0.1
0
Magnesium (Mg), % 8.0 to 10.5
0
Manganese (Mn), % 0 to 0.55
0 to 2.0
Nickel (Ni), % 0 to 0.1
9.0 to 13
Niobium (Nb), % 0
0 to 1.0
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 2.5
0 to 0.75
Sulfur (S), % 0
0 to 0.030
Tin (Sn), % 0 to 0.1
0
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0