MakeItFrom.com
Menu (ESC)

2219 Aluminum vs. N07716 Nickel

2219 aluminum belongs to the aluminum alloys classification, while N07716 nickel belongs to the nickel alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 N07716 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 2.2 to 20
34
Fatigue Strength, MPa 90 to 130
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
78
Shear Strength, MPa 110 to 280
580
Tensile Strength: Ultimate (UTS), MPa 180 to 480
860
Tensile Strength: Yield (Proof), MPa 88 to 390
350

Thermal Properties

Latent Heat of Fusion, J/g 390
320
Maximum Temperature: Mechanical, °C 230
980
Melting Completion (Liquidus), °C 640
1480
Melting Onset (Solidus), °C 540
1430
Specific Heat Capacity, J/kg-K 870
440
Thermal Conductivity, W/m-K 110 to 170
11
Thermal Expansion, µm/m-K 22
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 28 to 44
1.4
Electrical Conductivity: Equal Weight (Specific), % IACS 81 to 130
1.5

Otherwise Unclassified Properties

Base Metal Price, % relative 11
75
Density, g/cm3 3.1
8.5
Embodied Carbon, kg CO2/kg material 8.2
13
Embodied Energy, MJ/kg 150
190
Embodied Water, L/kg 1130
280

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.6 to 60
240
Resilience: Unit (Modulus of Resilience), kJ/m3 54 to 1060
300
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 44
23
Strength to Weight: Axial, points 16 to 43
28
Strength to Weight: Bending, points 23 to 44
24
Thermal Diffusivity, mm2/s 42 to 63
2.8
Thermal Shock Resistance, points 8.2 to 22
24

Alloy Composition

Aluminum (Al), % 91.5 to 93.8
0 to 0.35
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
19 to 22
Copper (Cu), % 5.8 to 6.8
0
Iron (Fe), % 0 to 0.3
0 to 11.3
Magnesium (Mg), % 0 to 0.020
0
Manganese (Mn), % 0.2 to 0.4
0 to 0.2
Molybdenum (Mo), % 0
7.0 to 9.5
Nickel (Ni), % 0
59 to 63
Niobium (Nb), % 0
2.8 to 4.0
Phosphorus (P), % 0
0 to 0.015
Silicon (Si), % 0 to 0.2
0 to 0.2
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.020 to 0.1
1.0 to 1.6
Vanadium (V), % 0.050 to 0.15
0
Zinc (Zn), % 0 to 0.1
0
Zirconium (Zr), % 0.1 to 0.25
0
Residuals, % 0 to 0.15
0