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R58150 Titanium vs. 328.0 Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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