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EN AC-48100 Aluminum vs. EN 1.4105 Stainless Steel

EN AC-48100 aluminum belongs to the aluminum alloys classification, while EN 1.4105 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-48100 aluminum and the bottom bar is EN 1.4105 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 140
180
Elastic (Young's, Tensile) Modulus, GPa 76
200
Elongation at Break, % 1.1
23
Fatigue Strength, MPa 120 to 130
190
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 29
77
Tensile Strength: Ultimate (UTS), MPa 240 to 330
530
Tensile Strength: Yield (Proof), MPa 190 to 300
290

Thermal Properties

Latent Heat of Fusion, J/g 640
290
Maximum Temperature: Mechanical, °C 170
870
Melting Completion (Liquidus), °C 580
1430
Melting Onset (Solidus), °C 470
1390
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 130
25
Thermal Expansion, µm/m-K 20
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
2.5
Electrical Conductivity: Equal Weight (Specific), % IACS 87
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.0
Density, g/cm3 2.8
7.7
Embodied Carbon, kg CO2/kg material 7.3
2.2
Embodied Energy, MJ/kg 130
31
Embodied Water, L/kg 940
120

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.3 to 3.6
100
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
210
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
25
Strength to Weight: Axial, points 24 to 33
19
Strength to Weight: Bending, points 31 to 38
19
Thermal Diffusivity, mm2/s 55
6.7
Thermal Shock Resistance, points 11 to 16
19

Alloy Composition


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Aluminum (Al), % 72.1 to 79.8
0
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0
16 to 18
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.3
77.9 to 83.7
Magnesium (Mg), % 0.25 to 0.65
0
Manganese (Mn), % 0 to 0.5
0 to 1.5
Molybdenum (Mo), % 0
0.2 to 0.6
Nickel (Ni), % 0 to 0.3
0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 16 to 18
0 to 1.5
Sulfur (S), % 0
0.15 to 0.35
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.25
0