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7175 Aluminum vs. EN 2.4856 Nickel

7175 aluminum belongs to the aluminum alloys classification, while EN 2.4856 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 7175 aluminum and the bottom bar is EN 2.4856 nickel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
200
Elongation at Break, % 3.8 to 5.9
28
Fatigue Strength, MPa 150 to 180
280
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 26
79
Shear Strength, MPa 290 to 330
570
Tensile Strength: Ultimate (UTS), MPa 520 to 570
880
Tensile Strength: Yield (Proof), MPa 430 to 490
430

Thermal Properties

Latent Heat of Fusion, J/g 380
330
Maximum Temperature: Mechanical, °C 180
1000
Melting Completion (Liquidus), °C 640
1480
Melting Onset (Solidus), °C 480
1430
Specific Heat Capacity, J/kg-K 870
440
Thermal Conductivity, W/m-K 140
10
Thermal Expansion, µm/m-K 23
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
1.3
Electrical Conductivity: Equal Weight (Specific), % IACS 99
1.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
80
Density, g/cm3 3.0
8.6
Embodied Carbon, kg CO2/kg material 8.2
14
Embodied Energy, MJ/kg 150
190
Embodied Water, L/kg 1130
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 18 to 29
200
Resilience: Unit (Modulus of Resilience), kJ/m3 1310 to 1730
440
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 46
23
Strength to Weight: Axial, points 48 to 52
28
Strength to Weight: Bending, points 48 to 51
24
Thermal Diffusivity, mm2/s 53
2.7
Thermal Shock Resistance, points 23 to 25
29

Alloy Composition

Aluminum (Al), % 88 to 91.4
0 to 0.4
Carbon (C), % 0
0.030 to 0.1
Chromium (Cr), % 0.18 to 0.28
20 to 23
Cobalt (Co), % 0
0 to 1.0
Copper (Cu), % 1.2 to 2.0
0 to 0.5
Iron (Fe), % 0 to 0.2
0 to 5.0
Magnesium (Mg), % 2.1 to 2.9
0
Manganese (Mn), % 0 to 0.1
0 to 0.5
Molybdenum (Mo), % 0
8.0 to 10
Nickel (Ni), % 0
58 to 68.8
Niobium (Nb), % 0
3.2 to 4.2
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.15
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.1
0 to 0.4
Zinc (Zn), % 5.1 to 6.1
0
Residuals, % 0 to 0.15
0