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EN AC-51300 Aluminum vs. Titanium 6-7

EN AC-51300 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 (7, in this case) are not shown.

For each property being compared, the top bar is EN AC-51300 aluminum and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 67
120
Elongation at Break, % 3.7
11
Fatigue Strength, MPa 78
530
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 25
45
Tensile Strength: Ultimate (UTS), MPa 190
1020
Tensile Strength: Yield (Proof), MPa 110
900

Thermal Properties

Latent Heat of Fusion, J/g 400
410
Maximum Temperature: Mechanical, °C 170
300
Melting Completion (Liquidus), °C 640
1700
Melting Onset (Solidus), °C 600
1650
Specific Heat Capacity, J/kg-K 910
520
Thermal Expansion, µm/m-K 24
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 9.1
34
Embodied Energy, MJ/kg 150
540
Embodied Water, L/kg 1180
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 6.1
110
Resilience: Unit (Modulus of Resilience), kJ/m3 87
3460
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 20
56
Strength to Weight: Bending, points 28
44
Thermal Shock Resistance, points 8.6
66

Alloy Composition

Aluminum (Al), % 91.4 to 95.5
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 0.55
0 to 0.25
Magnesium (Mg), % 4.5 to 6.5
0
Manganese (Mn), % 0 to 0.45
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 0.55
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