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EN 1.4029 Stainless Steel vs. EN AC-42200 Aluminum

EN 1.4029 stainless steel belongs to the iron alloys classification, while EN AC-42200 aluminum belongs to the aluminum 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 EN 1.4029 stainless steel and the bottom bar is EN AC-42200 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 10 to 20
3.0 to 6.7
Fatigue Strength, MPa 270 to 400
86 to 90
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
26
Tensile Strength: Ultimate (UTS), MPa 700 to 930
320
Tensile Strength: Yield (Proof), MPa 410 to 740
240 to 260

Thermal Properties

Latent Heat of Fusion, J/g 270
500
Maximum Temperature: Mechanical, °C 750
170
Melting Completion (Liquidus), °C 1440
610
Melting Onset (Solidus), °C 1400
600
Specific Heat Capacity, J/kg-K 480
910
Thermal Conductivity, W/m-K 30
150
Thermal Expansion, µm/m-K 10
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 3.1
40
Electrical Conductivity: Equal Weight (Specific), % IACS 3.7
140

Otherwise Unclassified Properties

Base Metal Price, % relative 7.0
9.5
Density, g/cm3 7.7
2.6
Embodied Carbon, kg CO2/kg material 2.0
8.0
Embodied Energy, MJ/kg 28
150
Embodied Water, L/kg 100
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 89 to 120
9.0 to 20
Resilience: Unit (Modulus of Resilience), kJ/m3 440 to 1410
410 to 490
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
53
Strength to Weight: Axial, points 25 to 33
34 to 35
Strength to Weight: Bending, points 23 to 27
40 to 41
Thermal Diffusivity, mm2/s 8.1
66
Thermal Shock Resistance, points 26 to 34
15

Alloy Composition

Aluminum (Al), % 0
91 to 93.1
Carbon (C), % 0.25 to 0.32
0
Chromium (Cr), % 12 to 13.5
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 82.8 to 87.6
0 to 0.19
Magnesium (Mg), % 0
0.45 to 0.7
Manganese (Mn), % 0 to 1.5
0 to 0.1
Molybdenum (Mo), % 0 to 0.6
0
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0 to 1.0
6.5 to 7.5
Sulfur (S), % 0.15 to 0.25
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.070
Residuals, % 0
0 to 0.1