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2618 Aluminum vs. R58150 Titanium

2618 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium alloys. There are 26 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is 2618 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
140
Elongation at Break, % 5.8
13
Fatigue Strength, MPa 110
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 27
52
Shear Strength, MPa 260
470
Tensile Strength: Ultimate (UTS), MPa 420
770
Tensile Strength: Yield (Proof), MPa 350
550

Thermal Properties

Latent Heat of Fusion, J/g 390
410
Maximum Temperature: Mechanical, °C 210
320
Melting Completion (Liquidus), °C 640
1760
Melting Onset (Solidus), °C 550
1700
Specific Heat Capacity, J/kg-K 880
500
Thermal Expansion, µm/m-K 22
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
48
Density, g/cm3 2.9
5.4
Embodied Carbon, kg CO2/kg material 8.3
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1150
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23
94
Resilience: Unit (Modulus of Resilience), kJ/m3 850
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 47
32
Strength to Weight: Axial, points 40
40
Strength to Weight: Bending, points 42
35
Thermal Shock Resistance, points 19
48

Alloy Composition


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Aluminum (Al), % 92.4 to 94.9
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 1.9 to 2.7
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0.9 to 1.3
0 to 0.1
Magnesium (Mg), % 1.3 to 1.8
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0.9 to 1.2
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0.1 to 0.25
0
Titanium (Ti), % 0.040 to 0.1
83.5 to 86
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0