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6013 Aluminum vs. ASTM A182 Grade F23

6013 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F23 belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 6013 aluminum and the bottom bar is ASTM A182 grade F23.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 69
190
Elongation at Break, % 3.4 to 22
22
Fatigue Strength, MPa 98 to 140
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 190 to 240
360
Tensile Strength: Ultimate (UTS), MPa 310 to 410
570
Tensile Strength: Yield (Proof), MPa 170 to 350
460

Thermal Properties

Latent Heat of Fusion, J/g 410
250
Maximum Temperature: Mechanical, °C 160
450
Melting Completion (Liquidus), °C 650
1500
Melting Onset (Solidus), °C 580
1450
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
41
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 38
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 2.8
8.0
Embodied Carbon, kg CO2/kg material 8.3
2.5
Embodied Energy, MJ/kg 150
36
Embodied Water, L/kg 1170
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 13 to 58
120
Resilience: Unit (Modulus of Resilience), kJ/m3 200 to 900
550
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 31 to 41
20
Strength to Weight: Bending, points 37 to 44
19
Thermal Diffusivity, mm2/s 60
11
Thermal Shock Resistance, points 14 to 18
17

Alloy Composition


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Aluminum (Al), % 94.8 to 97.8
0 to 0.030
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0 to 0.1
1.9 to 2.6
Copper (Cu), % 0.6 to 1.1
0
Iron (Fe), % 0 to 0.5
93.2 to 96.2
Magnesium (Mg), % 0.8 to 1.2
0
Manganese (Mn), % 0.2 to 0.8
0.1 to 0.6
Molybdenum (Mo), % 0
0.050 to 0.3
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.020 to 0.080
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0.6 to 1.0
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0.0050 to 0.060
Tungsten (W), % 0
1.5 to 1.8
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0