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C355.0 Aluminum vs. Titanium 6-7

C355.0 aluminum belongs to the aluminum alloys classification, while titanium 6-7 belongs to the titanium alloys. There are 25 material properties with values for both materials. Properties with values for just one material (8, in this case) are not shown.

For each property being compared, the top bar is C355.0 aluminum and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
120
Elongation at Break, % 2.7 to 3.8
11
Fatigue Strength, MPa 76 to 84
530
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
45
Tensile Strength: Ultimate (UTS), MPa 290 to 310
1020
Tensile Strength: Yield (Proof), MPa 200 to 230
900

Thermal Properties

Latent Heat of Fusion, J/g 470
410
Maximum Temperature: Mechanical, °C 170
300
Melting Completion (Liquidus), °C 620
1700
Melting Onset (Solidus), °C 570
1650
Specific Heat Capacity, J/kg-K 900
520
Thermal Expansion, µm/m-K 22
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
75
Density, g/cm3 2.7
5.1
Embodied Carbon, kg CO2/kg material 8.0
34
Embodied Energy, MJ/kg 150
540
Embodied Water, L/kg 1120
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.5 to 9.8
110
Resilience: Unit (Modulus of Resilience), kJ/m3 290 to 380
3460
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 30 to 32
56
Strength to Weight: Bending, points 36 to 37
44
Thermal Shock Resistance, points 13 to 14
66

Alloy Composition


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Aluminum (Al), % 91.7 to 94.1
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Copper (Cu), % 1.0 to 1.5
0
Hydrogen (H), % 0
0 to 0.0090
Iron (Fe), % 0 to 0.2
0 to 0.25
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.1
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), % 4.5 to 5.5
0
Tantalum (Ta), % 0
0 to 0.5
Titanium (Ti), % 0 to 0.2
84.9 to 88
Zinc (Zn), % 0 to 0.1
0
Residuals, % 0 to 0.15
0