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328.0 Aluminum vs. R58150 Titanium

328.0 aluminum belongs to the aluminum alloys classification, while R58150 titanium 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 328.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 72
140
Elongation at Break, % 1.6 to 2.1
13
Fatigue Strength, MPa 55 to 80
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 27
52
Tensile Strength: Ultimate (UTS), MPa 200 to 270
770
Tensile Strength: Yield (Proof), MPa 120 to 170
550

Thermal Properties

Latent Heat of Fusion, J/g 510
410
Maximum Temperature: Mechanical, °C 180
320
Melting Completion (Liquidus), °C 620
1760
Melting Onset (Solidus), °C 560
1700
Specific Heat Capacity, J/kg-K 890
500
Thermal Expansion, µm/m-K 22
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 10
48
Density, g/cm3 2.7
5.4
Embodied Carbon, kg CO2/kg material 7.8
31
Embodied Energy, MJ/kg 140
480
Embodied Water, L/kg 1070
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.8 to 5.0
94
Resilience: Unit (Modulus of Resilience), kJ/m3 92 to 200
1110
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 21 to 28
40
Strength to Weight: Bending, points 28 to 34
35
Thermal Shock Resistance, points 9.2 to 12
48

Alloy Composition


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Aluminum (Al), % 84.5 to 91.1
0
Carbon (C), % 0
0 to 0.1
Chromium (Cr), % 0 to 0.35
0
Copper (Cu), % 1.0 to 2.0
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 1.0
0 to 0.1
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0.2 to 0.6
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 0 to 0.25
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 7.5 to 8.5
0
Titanium (Ti), % 0 to 0.25
83.5 to 86
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.5
0