MakeItFrom.com
Menu (ESC)

EN 2.4856 Nickel vs. 6351 Aluminum

EN 2.4856 nickel belongs to the nickel alloys classification, while 6351 aluminum belongs to the aluminum 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 EN 2.4856 nickel and the bottom bar is 6351 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 28
7.8 to 18
Fatigue Strength, MPa 280
79 to 130
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 79
26
Shear Strength, MPa 570
84 to 200
Tensile Strength: Ultimate (UTS), MPa 880
140 to 310
Tensile Strength: Yield (Proof), MPa 430
95 to 270

Thermal Properties

Latent Heat of Fusion, J/g 330
410
Maximum Temperature: Mechanical, °C 1000
160
Melting Completion (Liquidus), °C 1480
650
Melting Onset (Solidus), °C 1430
570
Specific Heat Capacity, J/kg-K 440
900
Thermal Conductivity, W/m-K 10
180
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.3
46
Electrical Conductivity: Equal Weight (Specific), % IACS 1.4
150

Otherwise Unclassified Properties

Base Metal Price, % relative 80
9.5
Density, g/cm3 8.6
2.7
Embodied Carbon, kg CO2/kg material 14
8.3
Embodied Energy, MJ/kg 190
150
Embodied Water, L/kg 290
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 200
20 to 38
Resilience: Unit (Modulus of Resilience), kJ/m3 440
65 to 540
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 23
50
Strength to Weight: Axial, points 28
14 to 32
Strength to Weight: Bending, points 24
22 to 38
Thermal Diffusivity, mm2/s 2.7
72
Thermal Shock Resistance, points 29
6.1 to 14

Alloy Composition

Aluminum (Al), % 0 to 0.4
96 to 98.5
Carbon (C), % 0.030 to 0.1
0
Chromium (Cr), % 20 to 23
0
Cobalt (Co), % 0 to 1.0
0
Copper (Cu), % 0 to 0.5
0 to 0.1
Iron (Fe), % 0 to 5.0
0 to 0.5
Magnesium (Mg), % 0
0.4 to 0.8
Manganese (Mn), % 0 to 0.5
0.4 to 0.8
Molybdenum (Mo), % 8.0 to 10
0
Nickel (Ni), % 58 to 68.8
0
Niobium (Nb), % 3.2 to 4.2
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0 to 0.5
0.7 to 1.3
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0 to 0.4
0 to 0.2
Zinc (Zn), % 0
0 to 0.2
Residuals, % 0
0 to 0.15