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5026 Aluminum vs. ASTM A182 Grade F24

5026 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F24 belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 5026 aluminum and the bottom bar is ASTM A182 grade F24.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 5.1 to 11
23
Fatigue Strength, MPa 94 to 140
330
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
74
Shear Strength, MPa 150 to 180
420
Tensile Strength: Ultimate (UTS), MPa 260 to 320
670
Tensile Strength: Yield (Proof), MPa 120 to 250
460

Thermal Properties

Latent Heat of Fusion, J/g 400
260
Maximum Temperature: Mechanical, °C 210
460
Melting Completion (Liquidus), °C 650
1470
Melting Onset (Solidus), °C 510
1430
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 130
39
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 31
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 99
8.8

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
4.0
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.9
2.3
Embodied Energy, MJ/kg 150
33
Embodied Water, L/kg 1150
61

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 15 to 29
140
Resilience: Unit (Modulus of Resilience), kJ/m3 100 to 440
570
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 49
24
Strength to Weight: Axial, points 26 to 32
24
Strength to Weight: Bending, points 33 to 37
22
Thermal Diffusivity, mm2/s 52
11
Thermal Shock Resistance, points 11 to 14
19

Alloy Composition

Aluminum (Al), % 88.2 to 94.7
0 to 0.020
Boron (B), % 0
0.0015 to 0.0070
Carbon (C), % 0
0.050 to 0.1
Chromium (Cr), % 0 to 0.3
2.2 to 2.6
Copper (Cu), % 0.1 to 0.8
0
Iron (Fe), % 0.2 to 1.0
94.5 to 96.1
Magnesium (Mg), % 3.9 to 4.9
0
Manganese (Mn), % 0.6 to 1.8
0.3 to 0.7
Molybdenum (Mo), % 0
0.9 to 1.1
Nitrogen (N), % 0
0 to 0.12
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0.55 to 1.4
0.15 to 0.45
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.2
0.060 to 0.1
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 1.0
0
Zirconium (Zr), % 0 to 0.3
0
Residuals, % 0 to 0.15
0