MakeItFrom.com
Menu (ESC)

N07716 Nickel vs. 6016 Aluminum

N07716 nickel belongs to the nickel alloys classification, while 6016 aluminum belongs to the aluminum 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 N07716 nickel and the bottom bar is 6016 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 34
11 to 27
Fatigue Strength, MPa 690
68 to 89
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 78
26
Shear Strength, MPa 580
130 to 170
Tensile Strength: Ultimate (UTS), MPa 860
200 to 280
Tensile Strength: Yield (Proof), MPa 350
110 to 210

Thermal Properties

Latent Heat of Fusion, J/g 320
410
Maximum Temperature: Mechanical, °C 980
160
Melting Completion (Liquidus), °C 1480
660
Melting Onset (Solidus), °C 1430
610
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 11
190 to 210
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.4
48 to 54
Electrical Conductivity: Equal Weight (Specific), % IACS 1.5
160 to 180

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 8.5
2.7
Embodied Carbon, kg CO2/kg material 13
8.2
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 280
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 240
29 to 47
Resilience: Unit (Modulus of Resilience), kJ/m3 300
82 to 340
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
51
Strength to Weight: Axial, points 28
21 to 29
Strength to Weight: Bending, points 24
29 to 35
Thermal Diffusivity, mm2/s 2.8
77 to 86
Thermal Shock Resistance, points 24
9.1 to 12

Alloy Composition


Deprecated: Automatic conversion of false to array is deprecated in /home/public/compare.php on line 460
Aluminum (Al), % 0 to 0.35
96.4 to 98.8
Carbon (C), % 0 to 0.030
0
Chromium (Cr), % 19 to 22
0 to 0.1
Copper (Cu), % 0
0 to 0.2
Iron (Fe), % 0 to 11.3
0 to 0.5
Magnesium (Mg), % 0
0.25 to 0.6
Manganese (Mn), % 0 to 0.2
0 to 0.2
Molybdenum (Mo), % 7.0 to 9.5
0
Nickel (Ni), % 59 to 63
0
Niobium (Nb), % 2.8 to 4.0
0
Phosphorus (P), % 0 to 0.015
0
Silicon (Si), % 0 to 0.2
1.0 to 1.5
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 1.0 to 1.6
0 to 0.15
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15