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Titanium 6-7 vs. B535.0 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while B535.0 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 B535.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
66
Elongation at Break, % 11
10
Fatigue Strength, MPa 530
62
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
25
Shear Strength, MPa 610
210
Tensile Strength: Ultimate (UTS), MPa 1020
260
Tensile Strength: Yield (Proof), MPa 900
130

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 300
170
Melting Completion (Liquidus), °C 1700
630
Melting Onset (Solidus), °C 1650
550
Specific Heat Capacity, J/kg-K 520
910
Thermal Expansion, µm/m-K 9.3
25

Otherwise Unclassified Properties

Base Metal Price, % relative 75
9.5
Density, g/cm3 5.1
2.6
Embodied Carbon, kg CO2/kg material 34
9.4
Embodied Energy, MJ/kg 540
160
Embodied Water, L/kg 190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
22
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
130
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 32
51
Strength to Weight: Axial, points 56
28
Strength to Weight: Bending, points 44
35
Thermal Shock Resistance, points 66
11

Alloy Composition

Aluminum (Al), % 5.5 to 6.5
91.7 to 93.4
Carbon (C), % 0 to 0.080
0
Copper (Cu), % 0
0 to 0.1
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.15
Magnesium (Mg), % 0
6.5 to 7.5
Manganese (Mn), % 0
0 to 0.050
Molybdenum (Mo), % 6.5 to 7.5
0
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 0.15
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0.1 to 0.25
Residuals, % 0
0 to 0.15