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AWS E320LR vs. 6025 Aluminum

AWS E320LR belongs to the iron alloys classification, while 6025 aluminum belongs to the aluminum alloys. There are 20 material properties with values for both materials. Properties with values for just one material (11, 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 AWS E320LR and the bottom bar is 6025 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
70
Elongation at Break, % 34
2.8 to 10
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Tensile Strength: Ultimate (UTS), MPa 580
190 to 240

Thermal Properties

Latent Heat of Fusion, J/g 300
410
Melting Completion (Liquidus), °C 1410
650
Melting Onset (Solidus), °C 1360
550
Specific Heat Capacity, J/kg-K 460
900
Thermal Expansion, µm/m-K 14
23

Otherwise Unclassified Properties

Base Metal Price, % relative 36
9.5
Density, g/cm3 8.2
2.8
Embodied Carbon, kg CO2/kg material 6.2
8.5
Embodied Energy, MJ/kg 87
150
Embodied Water, L/kg 220
1160

Common Calculations

Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
50
Strength to Weight: Axial, points 20
19 to 24
Strength to Weight: Bending, points 19
26 to 31
Thermal Shock Resistance, points 15
8.2 to 10

Alloy Composition

Aluminum (Al), % 0
91.7 to 96.3
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 19 to 21
0 to 0.2
Copper (Cu), % 3.0 to 4.0
0.2 to 0.7
Iron (Fe), % 32.7 to 42.5
0 to 0.7
Magnesium (Mg), % 0
2.1 to 3.0
Manganese (Mn), % 1.5 to 2.5
0.6 to 1.4
Molybdenum (Mo), % 2.0 to 3.0
0
Nickel (Ni), % 32 to 36
0
Niobium (Nb), % 0 to 0.4
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.3
0.8 to 1.5
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.2
Zinc (Zn), % 0
0 to 0.5
Residuals, % 0
0 to 0.15