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B535.0 Aluminum vs. 5652 Aluminum

Both B535.0 aluminum and 5652 aluminum are aluminum alloys. They have a very high 95% of their average alloy composition in common.

For each property being compared, the top bar is B535.0 aluminum and the bottom bar is 5652 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 65
47 to 77
Elastic (Young's, Tensile) Modulus, GPa 66
68
Elongation at Break, % 10
6.8 to 25
Fatigue Strength, MPa 62
60 to 140
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 25
26
Shear Strength, MPa 210
110 to 170
Tensile Strength: Ultimate (UTS), MPa 260
190 to 290
Tensile Strength: Yield (Proof), MPa 130
74 to 260

Thermal Properties

Latent Heat of Fusion, J/g 390
400
Maximum Temperature: Mechanical, °C 170
190
Melting Completion (Liquidus), °C 630
650
Melting Onset (Solidus), °C 550
610
Specific Heat Capacity, J/kg-K 910
900
Thermal Conductivity, W/m-K 96
140
Thermal Expansion, µm/m-K 25
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 24
35
Electrical Conductivity: Equal Weight (Specific), % IACS 82
120

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
9.5
Density, g/cm3 2.6
2.7
Embodied Carbon, kg CO2/kg material 9.4
8.6
Embodied Energy, MJ/kg 160
150
Embodied Water, L/kg 1180
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 22
12 to 39
Resilience: Unit (Modulus of Resilience), kJ/m3 130
40 to 480
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 51
51
Strength to Weight: Axial, points 28
20 to 30
Strength to Weight: Bending, points 35
27 to 36
Thermal Diffusivity, mm2/s 40
57
Thermal Shock Resistance, points 11
8.4 to 13

Alloy Composition

Aluminum (Al), % 91.7 to 93.4
95.8 to 97.7
Chromium (Cr), % 0
0.15 to 0.35
Copper (Cu), % 0 to 0.1
0 to 0.040
Iron (Fe), % 0 to 0.15
0 to 0.4
Magnesium (Mg), % 6.5 to 7.5
2.2 to 2.8
Manganese (Mn), % 0 to 0.050
0 to 0.010
Silicon (Si), % 0 to 0.15
0 to 0.4
Titanium (Ti), % 0.1 to 0.25
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15