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EN 1.4107 Stainless Steel vs. 336.0 Aluminum

EN 1.4107 stainless steel belongs to the iron alloys classification, while 336.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 1.4107 stainless steel and the bottom bar is 336.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
75
Elongation at Break, % 18 to 21
0.5
Fatigue Strength, MPa 260 to 350
80 to 93
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 76
28
Tensile Strength: Ultimate (UTS), MPa 620 to 700
250 to 320
Tensile Strength: Yield (Proof), MPa 400 to 570
190 to 300

Thermal Properties

Latent Heat of Fusion, J/g 270
570
Maximum Temperature: Mechanical, °C 740
210
Melting Completion (Liquidus), °C 1450
570
Melting Onset (Solidus), °C 1410
540
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 27
120
Thermal Expansion, µm/m-K 10
19

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.9
29
Electrical Conductivity: Equal Weight (Specific), % IACS 3.3
95

Otherwise Unclassified Properties

Base Metal Price, % relative 7.5
11
Density, g/cm3 7.8
2.8
Embodied Carbon, kg CO2/kg material 2.1
7.9
Embodied Energy, MJ/kg 30
140
Embodied Water, L/kg 100
1010

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110 to 120
1.1 to 1.6
Resilience: Unit (Modulus of Resilience), kJ/m3 420 to 840
250 to 580
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 22 to 25
25 to 32
Strength to Weight: Bending, points 21 to 22
32 to 38
Thermal Diffusivity, mm2/s 7.2
48
Thermal Shock Resistance, points 22 to 25
12 to 16

Alloy Composition

Aluminum (Al), % 0
79.1 to 85.8
Carbon (C), % 0 to 0.1
0
Chromium (Cr), % 11.5 to 12.5
0
Copper (Cu), % 0 to 0.3
0.5 to 1.5
Iron (Fe), % 83.8 to 87.2
0 to 1.2
Magnesium (Mg), % 0
0.7 to 1.3
Manganese (Mn), % 0.5 to 0.8
0 to 0.35
Molybdenum (Mo), % 0 to 0.5
0
Nickel (Ni), % 0.8 to 1.5
2.0 to 3.0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.4
11 to 13
Sulfur (S), % 0 to 0.020
0
Titanium (Ti), % 0
0 to 0.25
Vanadium (V), % 0 to 0.080
0
Zinc (Zn), % 0
0 to 0.35

Comparable Variants