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319.0 Aluminum vs. EN 1.4913 Stainless Steel

319.0 aluminum belongs to the aluminum alloys classification, while EN 1.4913 stainless steel belongs to the iron alloys. There are 30 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 319.0 aluminum and the bottom bar is EN 1.4913 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 1.8 to 2.0
14 to 22
Fatigue Strength, MPa 76 to 80
320 to 480
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
75
Shear Strength, MPa 170 to 210
550 to 590
Tensile Strength: Ultimate (UTS), MPa 190 to 240
870 to 980
Tensile Strength: Yield (Proof), MPa 110 to 180
480 to 850

Thermal Properties

Latent Heat of Fusion, J/g 480
270
Maximum Temperature: Mechanical, °C 170
700
Melting Completion (Liquidus), °C 600
1460
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 110
24
Thermal Expansion, µm/m-K 22
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 84
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
9.0
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 7.7
2.9
Embodied Energy, MJ/kg 140
41
Embodied Water, L/kg 1080
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.3 to 3.9
130 to 160
Resilience: Unit (Modulus of Resilience), kJ/m3 88 to 220
600 to 1860
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 48
25
Strength to Weight: Axial, points 18 to 24
31 to 35
Strength to Weight: Bending, points 25 to 30
26 to 28
Thermal Diffusivity, mm2/s 44
6.5
Thermal Shock Resistance, points 8.6 to 11
31 to 34

Alloy Composition

Aluminum (Al), % 85.8 to 91.5
0 to 0.020
Boron (B), % 0
0 to 0.0015
Carbon (C), % 0
0.17 to 0.23
Chromium (Cr), % 0
10 to 11.5
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.0
84.5 to 88.3
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.4 to 0.9
Molybdenum (Mo), % 0
0.5 to 0.8
Nickel (Ni), % 0 to 0.35
0.2 to 0.6
Niobium (Nb), % 0
0.25 to 0.55
Nitrogen (N), % 0
0.050 to 0.1
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 5.5 to 6.5
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.1 to 0.3
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0