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5082 Aluminum vs. ASTM A182 Grade F911

5082 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F911 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 5082 aluminum and the bottom bar is ASTM A182 grade F911.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
190
Elongation at Break, % 1.1
20
Fatigue Strength, MPa 110 to 130
350
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
76
Shear Strength, MPa 210 to 230
430
Tensile Strength: Ultimate (UTS), MPa 380 to 400
690
Tensile Strength: Yield (Proof), MPa 300 to 340
500

Thermal Properties

Latent Heat of Fusion, J/g 400
270
Maximum Temperature: Mechanical, °C 180
600
Melting Completion (Liquidus), °C 640
1480
Melting Onset (Solidus), °C 560
1440
Specific Heat Capacity, J/kg-K 910
470
Thermal Conductivity, W/m-K 130
26
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 32
9.2
Electrical Conductivity: Equal Weight (Specific), % IACS 110
10

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.7
7.9
Embodied Carbon, kg CO2/kg material 8.9
2.8
Embodied Energy, MJ/kg 150
40
Embodied Water, L/kg 1180
90

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 4.0 to 4.3
130
Resilience: Unit (Modulus of Resilience), kJ/m3 670 to 870
650
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 39 to 41
24
Strength to Weight: Bending, points 43 to 45
22
Thermal Diffusivity, mm2/s 54
6.9
Thermal Shock Resistance, points 17 to 18
19

Alloy Composition

Aluminum (Al), % 93.5 to 96
0 to 0.020
Boron (B), % 0
0.00030 to 0.0060
Carbon (C), % 0
0.090 to 0.13
Chromium (Cr), % 0 to 0.15
8.5 to 9.5
Copper (Cu), % 0 to 0.15
0
Iron (Fe), % 0 to 0.35
86.2 to 88.9
Magnesium (Mg), % 4.0 to 5.0
0
Manganese (Mn), % 0 to 0.15
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.040 to 0.090
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.2
0.1 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.1
0 to 0.010
Tungsten (W), % 0
0.9 to 1.1
Vanadium (V), % 0
0.18 to 0.25
Zinc (Zn), % 0 to 0.25
0
Zirconium (Zr), % 0
0 to 0.010
Residuals, % 0 to 0.15
0