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4032 Aluminum vs. Titanium 6-7

4032 aluminum belongs to the aluminum alloys classification, while titanium 6-7 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 4032 aluminum and the bottom bar is titanium 6-7.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 73
120
Elongation at Break, % 6.7
11
Fatigue Strength, MPa 110
530
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 28
45
Shear Strength, MPa 260
610
Tensile Strength: Ultimate (UTS), MPa 390
1020
Tensile Strength: Yield (Proof), MPa 320
900

Thermal Properties

Latent Heat of Fusion, J/g 570
410
Maximum Temperature: Mechanical, °C 180
300
Melting Completion (Liquidus), °C 570
1700
Melting Onset (Solidus), °C 530
1650
Specific Heat Capacity, J/kg-K 900
520
Thermal Expansion, µm/m-K 19
9.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
75
Density, g/cm3 2.6
5.1
Embodied Carbon, kg CO2/kg material 7.8
34
Embodied Energy, MJ/kg 140
540
Embodied Water, L/kg 1030
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 25
110
Resilience: Unit (Modulus of Resilience), kJ/m3 700
3460
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 53
32
Strength to Weight: Axial, points 41
56
Strength to Weight: Bending, points 45
44
Thermal Shock Resistance, points 20
66

Alloy Composition

Aluminum (Al), % 81.1 to 87.2
5.5 to 6.5
Carbon (C), % 0
0 to 0.080
Chromium (Cr), % 0 to 0.1
0
Copper (Cu), % 0.5 to 1.3
0
Hydrogen (H), % 0
0 to 0.0090
Iron (Fe), % 0 to 1.0
0 to 0.25
Magnesium (Mg), % 0.8 to 1.3
0
Molybdenum (Mo), % 0
6.5 to 7.5
Nickel (Ni), % 0.5 to 1.3
0
Niobium (Nb), % 0
6.5 to 7.5
Nitrogen (N), % 0
0 to 0.050
Oxygen (O), % 0
0 to 0.2
Silicon (Si), % 11 to 13.5
0
Tantalum (Ta), % 0
0 to 0.5
Titanium (Ti), % 0
84.9 to 88
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0