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518.0 Aluminum vs. R58150 Titanium

518.0 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 518.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
140
Elongation at Break, % 5.0
13
Fatigue Strength, MPa 140
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 25
52
Shear Strength, MPa 200
470
Tensile Strength: Ultimate (UTS), MPa 310
770
Tensile Strength: Yield (Proof), MPa 190
550

Thermal Properties

Latent Heat of Fusion, J/g 390
410
Maximum Temperature: Mechanical, °C 170
320
Melting Completion (Liquidus), °C 620
1760
Melting Onset (Solidus), °C 560
1700
Specific Heat Capacity, J/kg-K 900
500
Thermal Expansion, µm/m-K 24
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
48
Density, g/cm3 2.7
5.4
Embodied Carbon, kg CO2/kg material 9.4
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1160
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14
94
Resilience: Unit (Modulus of Resilience), kJ/m3 270
1110
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 32
40
Strength to Weight: Bending, points 38
35
Thermal Shock Resistance, points 14
48

Alloy Composition


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Aluminum (Al), % 88.1 to 92.5
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0 to 0.25
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 1.8
0 to 0.1
Magnesium (Mg), % 7.5 to 8.5
0
Manganese (Mn), % 0 to 0.35
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0 to 0.15
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.35
0
Tin (Sn), % 0 to 0.15
0
Titanium (Ti), % 0
83.5 to 86
Zinc (Zn), % 0 to 0.15
0
Residuals, % 0 to 0.25
0