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R58150 Titanium vs. 319.0 Aluminum

R58150 titanium belongs to the titanium alloys classification, while 319.0 aluminum belongs to the aluminum alloys. There are 26 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 R58150 titanium and the bottom bar is 319.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 140
72
Elongation at Break, % 13
1.8 to 2.0
Fatigue Strength, MPa 330
76 to 80
Poisson's Ratio 0.32
0.33
Shear Modulus, GPa 52
27
Shear Strength, MPa 470
170 to 210
Tensile Strength: Ultimate (UTS), MPa 770
190 to 240
Tensile Strength: Yield (Proof), MPa 550
110 to 180

Thermal Properties

Latent Heat of Fusion, J/g 410
480
Maximum Temperature: Mechanical, °C 320
170
Melting Completion (Liquidus), °C 1760
600
Melting Onset (Solidus), °C 1700
540
Specific Heat Capacity, J/kg-K 500
880
Thermal Expansion, µm/m-K 8.4
22

Otherwise Unclassified Properties

Base Metal Price, % relative 48
10
Density, g/cm3 5.4
2.9
Embodied Carbon, kg CO2/kg material 31
7.7
Embodied Energy, MJ/kg 480
140
Embodied Water, L/kg 150
1080

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 94
3.3 to 3.9
Resilience: Unit (Modulus of Resilience), kJ/m3 1110
88 to 220
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 32
48
Strength to Weight: Axial, points 40
18 to 24
Strength to Weight: Bending, points 35
25 to 30
Thermal Shock Resistance, points 48
8.6 to 11

Alloy Composition

Aluminum (Al), % 0
85.8 to 91.5
Carbon (C), % 0 to 0.1
0
Copper (Cu), % 0
3.0 to 4.0
Hydrogen (H), % 0 to 0.015
0
Iron (Fe), % 0 to 0.1
0 to 1.0
Magnesium (Mg), % 0
0 to 0.1
Manganese (Mn), % 0
0 to 0.5
Molybdenum (Mo), % 14 to 16
0
Nickel (Ni), % 0
0 to 0.35
Nitrogen (N), % 0 to 0.050
0
Oxygen (O), % 0 to 0.2
0
Silicon (Si), % 0
5.5 to 6.5
Titanium (Ti), % 83.5 to 86
0 to 0.25
Zinc (Zn), % 0
0 to 1.0
Residuals, % 0
0 to 0.5