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5051A Aluminum vs. 6023 Aluminum

Both 5051A aluminum and 6023 aluminum are aluminum alloys. They have a very high 97% of their average alloy composition in common.

For each property being compared, the top bar is 5051A aluminum and the bottom bar is 6023 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 68
69
Elongation at Break, % 18 to 21
11
Fatigue Strength, MPa 51 to 61
120 to 130
Poisson's Ratio 0.33
0.33
Shear Modulus, GPa 26
26
Shear Strength, MPa 110
210 to 220
Tensile Strength: Ultimate (UTS), MPa 170
360
Tensile Strength: Yield (Proof), MPa 56
300 to 310

Thermal Properties

Latent Heat of Fusion, J/g 400
400
Maximum Temperature: Mechanical, °C 190
160
Melting Completion (Liquidus), °C 640
640
Melting Onset (Solidus), °C 610
580
Specific Heat Capacity, J/kg-K 900
890
Thermal Conductivity, W/m-K 150
170
Thermal Expansion, µm/m-K 23
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 39
45
Electrical Conductivity: Equal Weight (Specific), % IACS 130
140

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
11
Density, g/cm3 2.7
2.8
Embodied Carbon, kg CO2/kg material 8.5
8.3
Embodied Energy, MJ/kg 150
150
Embodied Water, L/kg 1190
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 24 to 27
38 to 39
Resilience: Unit (Modulus of Resilience), kJ/m3 23
670 to 690
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
49
Strength to Weight: Axial, points 17 to 18
35 to 36
Strength to Weight: Bending, points 25
40
Thermal Diffusivity, mm2/s 63
67
Thermal Shock Resistance, points 7.6
16

Alloy Composition

Aluminum (Al), % 96.1 to 98.6
94 to 97.7
Bismuth (Bi), % 0
0.3 to 0.8
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0 to 0.050
0.2 to 0.5
Iron (Fe), % 0 to 0.45
0 to 0.5
Magnesium (Mg), % 1.4 to 2.1
0.4 to 0.9
Manganese (Mn), % 0 to 0.25
0.2 to 0.6
Silicon (Si), % 0 to 0.3
0.6 to 1.4
Tin (Sn), % 0
0.6 to 1.2
Titanium (Ti), % 0 to 0.1
0
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0
0 to 0.15