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EN AC-51400 Aluminum vs. AISI 301LN Stainless Steel

EN AC-51400 aluminum belongs to the aluminum alloys classification, while AISI 301LN stainless steel belongs to the iron alloys. There are 30 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 EN AC-51400 aluminum and the bottom bar is AISI 301LN stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 71
210 to 320
Elastic (Young's, Tensile) Modulus, GPa 67
200
Elongation at Break, % 3.4
23 to 51
Fatigue Strength, MPa 85
270 to 520
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
77
Tensile Strength: Ultimate (UTS), MPa 190
630 to 1060
Tensile Strength: Yield (Proof), MPa 120
270 to 770

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 170
890
Melting Completion (Liquidus), °C 640
1430
Melting Onset (Solidus), °C 600
1380
Specific Heat Capacity, J/kg-K 910
480
Thermal Conductivity, W/m-K 110
15
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 110
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.1
2.7
Embodied Energy, MJ/kg 150
39
Embodied Water, L/kg 1170
130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.6
220 to 290
Resilience: Unit (Modulus of Resilience), kJ/m3 110
180 to 1520
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 20
22 to 38
Strength to Weight: Bending, points 28
21 to 30
Thermal Diffusivity, mm2/s 46
4.0
Thermal Shock Resistance, points 8.6
14 to 24

Alloy Composition

Aluminum (Al), % 90.5 to 95.5
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 0 to 0.050
0
Iron (Fe), % 0 to 0.55
70.7 to 77.9
Magnesium (Mg), % 4.5 to 6.5
0
Manganese (Mn), % 0 to 0.45
0 to 2.0
Nickel (Ni), % 0
6.0 to 8.0
Nitrogen (N), % 0
0.070 to 0.2
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 1.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.2
0
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0