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712.0 Aluminum vs. R58150 Titanium

712.0 aluminum belongs to the aluminum alloys classification, while R58150 titanium belongs to the titanium 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 712.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
140
Elongation at Break, % 4.5 to 4.7
13
Fatigue Strength, MPa 140 to 180
330
Poisson's Ratio 0.32
0.32
Shear Modulus, GPa 27
52
Shear Strength, MPa 180
470
Tensile Strength: Ultimate (UTS), MPa 250 to 260
770
Tensile Strength: Yield (Proof), MPa 180 to 200
550

Thermal Properties

Latent Heat of Fusion, J/g 380
410
Maximum Temperature: Mechanical, °C 190
320
Melting Completion (Liquidus), °C 640
1760
Melting Onset (Solidus), °C 610
1700
Specific Heat Capacity, J/kg-K 870
500
Thermal Expansion, µm/m-K 24
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
48
Density, g/cm3 3.0
5.4
Embodied Carbon, kg CO2/kg material 8.0
31
Embodied Energy, MJ/kg 150
480
Embodied Water, L/kg 1140
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 11
94
Resilience: Unit (Modulus of Resilience), kJ/m3 240 to 270
1110
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
32
Strength to Weight: Axial, points 24 to 25
40
Strength to Weight: Bending, points 30 to 31
35
Thermal Shock Resistance, points 11
48

Alloy Composition


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Aluminum (Al), % 90.7 to 94
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0.4 to 0.6
0
Copper (Cu), % 0 to 0.25
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 0.5
0 to 0.1
Magnesium (Mg), % 0.5 to 0.65
0
Manganese (Mn), % 0 to 0.1
0
Molybdenum (Mo), % 0
14 to 16
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 0 to 0.3
0
Titanium (Ti), % 0.15 to 0.25
83.5 to 86
Zinc (Zn), % 5.0 to 6.5
0
Residuals, % 0 to 0.2
0