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336.0 Aluminum vs. R58150 Titanium

336.0 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 (6, in this case) are not shown.

For each property being compared, the top bar is 336.0 aluminum and the bottom bar is R58150 titanium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 75
140
Elongation at Break, % 0.5
13
Fatigue Strength, MPa 80 to 93
330
Poisson's Ratio 0.33
0.32
Shear Modulus, GPa 28
52
Shear Strength, MPa 190 to 250
470
Tensile Strength: Ultimate (UTS), MPa 250 to 320
770
Tensile Strength: Yield (Proof), MPa 190 to 300
550

Thermal Properties

Latent Heat of Fusion, J/g 570
410
Maximum Temperature: Mechanical, °C 210
320
Melting Completion (Liquidus), °C 570
1760
Melting Onset (Solidus), °C 540
1700
Specific Heat Capacity, J/kg-K 890
500
Thermal Expansion, µm/m-K 19
8.4

Otherwise Unclassified Properties

Base Metal Price, % relative 11
48
Density, g/cm3 2.8
5.4
Embodied Carbon, kg CO2/kg material 7.9
31
Embodied Energy, MJ/kg 140
480
Embodied Water, L/kg 1010
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.1 to 1.6
94
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 580
1110
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
32
Strength to Weight: Axial, points 25 to 32
40
Strength to Weight: Bending, points 32 to 38
35
Thermal Shock Resistance, points 12 to 16
48

Alloy Composition

Aluminum (Al), % 79.1 to 85.8
0
Carbon (C), % 0
0 to 0.1
Copper (Cu), % 0.5 to 1.5
0
Hydrogen (H), % 0
0 to 0.015
Iron (Fe), % 0 to 1.2
0 to 0.1
Magnesium (Mg), % 0.7 to 1.3
0
Manganese (Mn), % 0 to 0.35
0
Molybdenum (Mo), % 0
14 to 16
Nickel (Ni), % 2.0 to 3.0
0
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 11 to 13
0
Titanium (Ti), % 0 to 0.25
83.5 to 86
Zinc (Zn), % 0 to 0.35
0