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Titanium 6-7 vs. 2036 Aluminum

Titanium 6-7 belongs to the titanium alloys classification, while 2036 aluminum belongs to the aluminum alloys. There are 26 material properties with values for both materials. Properties with values for just one material (5, in this case) are not shown.

For each property being compared, the top bar is titanium 6-7 and the bottom bar is 2036 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 120
70
Elongation at Break, % 11
24
Fatigue Strength, MPa 530
130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 45
26
Shear Strength, MPa 610
210
Tensile Strength: Ultimate (UTS), MPa 1020
340
Tensile Strength: Yield (Proof), MPa 900
200

Thermal Properties

Latent Heat of Fusion, J/g 410
390
Maximum Temperature: Mechanical, °C 300
190
Melting Completion (Liquidus), °C 1700
650
Melting Onset (Solidus), °C 1650
560
Specific Heat Capacity, J/kg-K 520
890
Thermal Expansion, µm/m-K 9.3
23

Otherwise Unclassified Properties

Base Metal Price, % relative 75
10
Density, g/cm3 5.1
2.9
Embodied Carbon, kg CO2/kg material 34
8.1
Embodied Energy, MJ/kg 540
150
Embodied Water, L/kg 190
1160

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
70
Resilience: Unit (Modulus of Resilience), kJ/m3 3460
270
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 32
48
Strength to Weight: Axial, points 56
33
Strength to Weight: Bending, points 44
38
Thermal Shock Resistance, points 66
15

Alloy Composition


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Aluminum (Al), % 5.5 to 6.5
94.4 to 97.4
Carbon (C), % 0 to 0.080
0
Chromium (Cr), % 0
0 to 0.1
Copper (Cu), % 0
2.2 to 3.0
Hydrogen (H), % 0 to 0.0090
0
Iron (Fe), % 0 to 0.25
0 to 0.5
Magnesium (Mg), % 0
0.3 to 0.6
Manganese (Mn), % 0
0.1 to 0.4
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 0.5
Tantalum (Ta), % 0 to 0.5
0
Titanium (Ti), % 84.9 to 88
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15