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B535.0 Aluminum vs. Titanium 6-7

B535.0 aluminum belongs to the aluminum alloys classification, while titanium 6-7 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 B535.0 aluminum and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition


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Aluminum (Al), % 91.7 to 93.4
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 0 to 0.1
0
Hydrogen (H), % 0
0 to 0.0090
Iron (Fe), % 0 to 0.15
0 to 0.25
Magnesium (Mg), % 6.5 to 7.5
0
Manganese (Mn), % 0 to 0.050
0
Molybdenum (Mo), % 0
6.5 to 7.5
Niobium (Nb), % 0
6.5 to 7.5
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.15
0
Tantalum (Ta), % 0
0 to 0.5
Titanium (Ti), % 0.1 to 0.25
84.9 to 88
Residuals, % 0 to 0.15
0