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Nickel 690 vs. 713.0 Aluminum

Nickel 690 belongs to the nickel alloys classification, while 713.0 aluminum belongs to the aluminum alloys. There are 31 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 nickel 690 and the bottom bar is 713.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 90
74 to 75
Elastic (Young's, Tensile) Modulus, GPa 200
71
Elongation at Break, % 3.4 to 34
3.9 to 4.3
Fatigue Strength, MPa 180 to 300
63 to 120
Poisson's Ratio 0.28
0.32
Shear Modulus, GPa 79
27
Shear Strength, MPa 420 to 570
180
Tensile Strength: Ultimate (UTS), MPa 640 to 990
240 to 260
Tensile Strength: Yield (Proof), MPa 250 to 760
170

Thermal Properties

Latent Heat of Fusion, J/g 320
370
Maximum Temperature: Mechanical, °C 1010
180
Melting Completion (Liquidus), °C 1380
630
Melting Onset (Solidus), °C 1340
610
Specific Heat Capacity, J/kg-K 470
860
Thermal Conductivity, W/m-K 14
150
Thermal Expansion, µm/m-K 14
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 1.5
35
Electrical Conductivity: Equal Weight (Specific), % IACS 1.6
100

Otherwise Unclassified Properties

Base Metal Price, % relative 50
9.5
Density, g/cm3 8.3
3.1
Embodied Carbon, kg CO2/kg material 8.2
7.8
Embodied Energy, MJ/kg 120
150
Embodied Water, L/kg 290
1110

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 31 to 170
8.7 to 9.9
Resilience: Unit (Modulus of Resilience), kJ/m3 160 to 1440
210 to 220
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 24
45
Strength to Weight: Axial, points 21 to 33
22 to 23
Strength to Weight: Bending, points 20 to 27
28 to 29
Thermal Diffusivity, mm2/s 3.5
57
Thermal Shock Resistance, points 16 to 25
10 to 11

Alloy Composition

Aluminum (Al), % 0
87.6 to 92.4
Carbon (C), % 0 to 0.050
0
Chromium (Cr), % 27 to 31
0 to 0.35
Copper (Cu), % 0 to 0.5
0.4 to 1.0
Iron (Fe), % 7.0 to 11
0 to 1.1
Magnesium (Mg), % 0
0.2 to 0.5
Manganese (Mn), % 0 to 0.5
0 to 0.6
Nickel (Ni), % 58 to 66
0 to 0.15
Silicon (Si), % 0 to 0.5
0 to 0.25
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
7.0 to 8.0
Residuals, % 0
0 to 0.25