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5383 Aluminum vs. EN 1.4374 Stainless Steel

5383 aluminum belongs to the aluminum alloys classification, while EN 1.4374 stainless steel belongs to the iron alloys. There are 32 material properties with values for both materials. Properties with values for just one material (2, 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 5383 aluminum and the bottom bar is EN 1.4374 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
230
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.7 to 15
40
Fatigue Strength, MPa 130 to 200
340
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
77
Shear Strength, MPa 190 to 220
550
Tensile Strength: Ultimate (UTS), MPa 310 to 370
800
Tensile Strength: Yield (Proof), MPa 150 to 310
400

Thermal Properties

Latent Heat of Fusion, J/g 390
290
Maximum Temperature: Corrosion, °C 65
410
Maximum Temperature: Mechanical, °C 200
920
Melting Completion (Liquidus), °C 650
1400
Melting Onset (Solidus), °C 540
1360
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 24
17

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
2.4
Electrical Conductivity: Equal Weight (Specific), % IACS 97
2.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
14
Density, g/cm3 2.7
7.7
Embodied Carbon, kg CO2/kg material 9.0
2.9
Embodied Energy, MJ/kg 160
42
Embodied Water, L/kg 1170
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
270
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
400
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 32 to 38
29
Strength to Weight: Bending, points 38 to 42
25
Thermal Diffusivity, mm2/s 51
4.0
Thermal Shock Resistance, points 14 to 16
17

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0.050 to 0.1
Chromium (Cr), % 0 to 0.25
17.5 to 18.5
Copper (Cu), % 0 to 0.2
0 to 0.4
Iron (Fe), % 0 to 0.25
63.5 to 67.9
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
9.0 to 10
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0
5.0 to 6.0
Nitrogen (N), % 0
0.25 to 0.32
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.25
0.3 to 0.6
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0