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2219 Aluminum vs. ASTM A387 Grade 91 Class 2

2219 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 91 class 2 belongs to the iron alloys. There are 30 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 2219 aluminum and the bottom bar is ASTM A387 grade 91 class 2.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 2.2 to 20
20
Fatigue Strength, MPa 90 to 130
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
75
Shear Strength, MPa 110 to 280
420
Tensile Strength: Ultimate (UTS), MPa 180 to 480
670
Tensile Strength: Yield (Proof), MPa 88 to 390
470

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Mechanical, °C 230
600
Melting Completion (Liquidus), °C 640
1460
Melting Onset (Solidus), °C 540
1420
Specific Heat Capacity, J/kg-K 870
470
Thermal Conductivity, W/m-K 110 to 170
26
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28 to 44
8.9
Electrical Conductivity: Equal Weight (Specific), % IACS 81 to 130
10

Otherwise Unclassified Properties

Base Metal Price, % relative 11
7.0
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
2.6
Embodied Energy, MJ/kg 150
37
Embodied Water, L/kg 1130
88

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.6 to 60
120
Resilience: Unit (Modulus of Resilience), kJ/m3 54 to 1060
580
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 44
25
Strength to Weight: Axial, points 16 to 43
24
Strength to Weight: Bending, points 23 to 44
22
Thermal Diffusivity, mm2/s 42 to 63
6.9
Thermal Shock Resistance, points 8.2 to 22
19

Alloy Composition


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Aluminum (Al), % 91.5 to 93.8
0 to 0.020
Carbon (C), % 0
0.080 to 0.12
Chromium (Cr), % 0
8.0 to 9.5
Copper (Cu), % 5.8 to 6.8
0
Iron (Fe), % 0 to 0.3
87.3 to 90.3
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0.2 to 0.4
0.3 to 0.6
Molybdenum (Mo), % 0
0.85 to 1.1
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.060 to 0.1
Nitrogen (N), % 0
0.030 to 0.070
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.2
0.2 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.020 to 0.1
0 to 0.010
Vanadium (V), % 0.050 to 0.15
0.18 to 0.25
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0.1 to 0.25
0 to 0.010
Residuals, % 0 to 0.15
0