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Titanium 6-7 vs. 518.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 518.0 aluminum belongs to the aluminum 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 titanium 6-7 and the bottom bar is 518.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
67
Elongation at Break, % 11
5.0
Fatigue Strength, MPa 530
140
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
25
Shear Strength, MPa 610
200
Tensile Strength: Ultimate (UTS), MPa 1020
310
Tensile Strength: Yield (Proof), MPa 900
190

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
620
Melting Onset (Solidus), °C 1650
560
Specific Heat Capacity, J/kg-K 520
900
Thermal Expansion, µm/m-K 9.3
24

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 5.1
2.7
Embodied Carbon, kg CO2/kg material 34
9.4
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
14
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
270
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 56
32
Strength to Weight: Bending, points 44
38
Thermal Shock Resistance, points 66
14

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
88.1 to 92.5
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
0 to 0.25
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 1.8
Magnesium (Mg), % 0
7.5 to 8.5
Manganese (Mn), % 0
0 to 0.35
Molybdenum (Mo), % 6.5 to 7.5
0
Nickel (Ni), % 0
0 to 0.15
Niobium (Nb), % 6.5 to 7.5
0
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
0 to 0.35
Tantalum (Ta), % 0 to 0.5
0
Tin (Sn), % 0
0 to 0.15
Titanium (Ti), % 84.9 to 88
0
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.25