MakeItFrom.com
Menu (ESC)

7050 Aluminum vs. N08026 Nickel

7050 aluminum belongs to the aluminum alloys classification, while N08026 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 7050 aluminum and the bottom bar is N08026 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 2.2 to 12
34
Fatigue Strength, MPa 130 to 210
200
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 26
80
Shear Strength, MPa 280 to 330
410
Tensile Strength: Ultimate (UTS), MPa 490 to 570
620
Tensile Strength: Yield (Proof), MPa 390 to 500
270

Thermal Properties

Latent Heat of Fusion, J/g 370
310
Maximum Temperature: Mechanical, °C 190
990
Melting Completion (Liquidus), °C 630
1430
Melting Onset (Solidus), °C 490
1380
Specific Heat Capacity, J/kg-K 860
460
Thermal Conductivity, W/m-K 140
12
Thermal Expansion, µm/m-K 24
15

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.6
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
41
Density, g/cm3 3.1
8.2
Embodied Carbon, kg CO2/kg material 8.2
7.2
Embodied Energy, MJ/kg 150
98
Embodied Water, L/kg 1120
240

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 10 to 55
170
Resilience: Unit (Modulus of Resilience), kJ/m3 1110 to 1760
180
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
24
Strength to Weight: Axial, points 45 to 51
21
Strength to Weight: Bending, points 45 to 50
20
Thermal Diffusivity, mm2/s 54
3.2
Thermal Shock Resistance, points 21 to 25
15

Alloy Composition

Aluminum (Al), % 87.3 to 92.1
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0 to 0.040
22 to 26
Copper (Cu), % 2.0 to 2.6
2.0 to 4.0
Iron (Fe), % 0 to 0.15
24.4 to 37.9
Magnesium (Mg), % 1.9 to 2.6
0
Manganese (Mn), % 0 to 0.1
0 to 1.0
Molybdenum (Mo), % 0
5.0 to 6.7
Nickel (Ni), % 0
33 to 37.2
Nitrogen (N), % 0
0.1 to 0.16
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.12
0 to 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.060
0
Zinc (Zn), % 5.7 to 6.7
0
Zirconium (Zr), % 0.080 to 0.15
0
Residuals, % 0 to 0.15
0