MakeItFrom.com
Menu (ESC)

EN AC-21100 Aluminum vs. EN 2.4816 Nickel

EN AC-21100 aluminum belongs to the aluminum alloys classification, while EN 2.4816 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 EN AC-21100 aluminum and the bottom bar is EN 2.4816 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 100 to 110
170
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 6.2 to 7.3
34
Fatigue Strength, MPa 79 to 87
200
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Tensile Strength: Ultimate (UTS), MPa 340 to 350
700
Tensile Strength: Yield (Proof), MPa 210 to 240
270

Thermal Properties

Latent Heat of Fusion, J/g 390
310
Maximum Temperature: Mechanical, °C 170
1150
Melting Completion (Liquidus), °C 670
1370
Melting Onset (Solidus), °C 550
1320
Specific Heat Capacity, J/kg-K 880
460
Thermal Conductivity, W/m-K 130
15
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 34
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 100
1.8

Otherwise Unclassified Properties

Base Metal Price, % relative 11
55
Density, g/cm3 3.0
8.5
Embodied Carbon, kg CO2/kg material 8.0
9.0
Embodied Energy, MJ/kg 150
130
Embodied Water, L/kg 1150
260

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 19 to 21
190
Resilience: Unit (Modulus of Resilience), kJ/m3 300 to 400
190
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
23
Strength to Weight: Axial, points 31 to 33
23
Strength to Weight: Bending, points 36 to 37
21
Thermal Diffusivity, mm2/s 48
3.8
Thermal Shock Resistance, points 15
20

Alloy Composition

Aluminum (Al), % 93.4 to 95.7
0 to 0.3
Carbon (C), % 0
0.050 to 0.1
Chromium (Cr), % 0
14 to 17
Copper (Cu), % 4.2 to 5.2
0 to 0.5
Iron (Fe), % 0 to 0.19
6.0 to 10
Manganese (Mn), % 0 to 0.55
0 to 1.0
Nickel (Ni), % 0
72 to 80
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.18
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0.15 to 0.3
0 to 0.3
Zinc (Zn), % 0 to 0.070
0
Residuals, % 0 to 0.1
0