MakeItFrom.com
Menu (ESC)

514.0 Aluminum vs. Nickel 690

514.0 aluminum belongs to the aluminum alloys classification, while nickel 690 belongs to the nickel 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 514.0 aluminum and the bottom bar is nickel 690.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 50
90
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 7.3
3.4 to 34
Fatigue Strength, MPa 48
180 to 300
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 25
79
Shear Strength, MPa 140
420 to 570
Tensile Strength: Ultimate (UTS), MPa 180
640 to 990
Tensile Strength: Yield (Proof), MPa 74
250 to 760

Thermal Properties

Latent Heat of Fusion, J/g 400
320
Maximum Temperature: Mechanical, °C 170
1010
Melting Completion (Liquidus), °C 640
1380
Melting Onset (Solidus), °C 610
1340
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 140
14
Thermal Expansion, µm/m-K 24
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.5
Electrical Conductivity: Equal Weight (Specific), % IACS 120
1.6

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
50
Density, g/cm3 2.7
8.3
Embodied Carbon, kg CO2/kg material 8.9
8.2
Embodied Energy, MJ/kg 150
120
Embodied Water, L/kg 1180
290

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
31 to 170
Resilience: Unit (Modulus of Resilience), kJ/m3 41
160 to 1440
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 19
21 to 33
Strength to Weight: Bending, points 26
20 to 27
Thermal Diffusivity, mm2/s 57
3.5
Thermal Shock Resistance, points 7.9
16 to 25

Alloy Composition

Aluminum (Al), % 93.6 to 96.5
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
27 to 31
Copper (Cu), % 0 to 0.15
0 to 0.5
Iron (Fe), % 0 to 0.5
7.0 to 11
Magnesium (Mg), % 3.5 to 4.5
0
Manganese (Mn), % 0 to 0.35
0 to 0.5
Nickel (Ni), % 0
58 to 66
Silicon (Si), % 0 to 0.35
0 to 0.5
Sulfur (S), % 0
0 to 0.015
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.15
0