MakeItFrom.com
Menu (ESC)

2218 Aluminum vs. ASTM A182 Grade F3V

2218 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F3V belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 2218 aluminum and the bottom bar is ASTM A182 grade F3V.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 95 to 110
210
Elastic (Young's, Tensile) Modulus, GPa 73
190
Elongation at Break, % 6.8 to 10
20
Fatigue Strength, MPa 110
330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 210 to 250
410
Tensile Strength: Ultimate (UTS), MPa 330 to 430
660
Tensile Strength: Yield (Proof), MPa 260 to 310
470

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 220
470
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 510
1430
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 140
39
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 37
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 110
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 11
4.2
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
2.3
Embodied Energy, MJ/kg 150
33
Embodied Water, L/kg 1130
63

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 27 to 31
120
Resilience: Unit (Modulus of Resilience), kJ/m3 450 to 650
590
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 30 to 39
23
Strength to Weight: Bending, points 34 to 41
21
Thermal Diffusivity, mm2/s 52
10
Thermal Shock Resistance, points 15 to 19
19

Alloy Composition

Aluminum (Al), % 88.8 to 93.6
0
Boron (B), % 0
0.0010 to 0.0030
Carbon (C), % 0
0.050 to 0.18
Chromium (Cr), % 0 to 0.1
2.8 to 3.2
Copper (Cu), % 3.5 to 4.5
0
Iron (Fe), % 0 to 1.0
94.4 to 95.7
Magnesium (Mg), % 1.2 to 1.8
0
Manganese (Mn), % 0 to 0.2
0.3 to 0.6
Molybdenum (Mo), % 0
0.9 to 1.1
Nickel (Ni), % 1.7 to 2.3
0
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.9
0 to 0.1
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0
0.015 to 0.035
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0