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358.0 Aluminum vs. ASTM A182 Grade F23

358.0 aluminum belongs to the aluminum alloys classification, while ASTM A182 grade F23 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 358.0 aluminum and the bottom bar is ASTM A182 grade F23.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 3.5 to 6.0
22
Fatigue Strength, MPa 100 to 110
320
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 300 to 320
360
Tensile Strength: Ultimate (UTS), MPa 350 to 370
570
Tensile Strength: Yield (Proof), MPa 290 to 320
460

Thermal Properties

Latent Heat of Fusion, J/g 520
250
Maximum Temperature: Mechanical, °C 170
450
Melting Completion (Liquidus), °C 600
1500
Melting Onset (Solidus), °C 560
1450
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 150
41
Thermal Expansion, µm/m-K 21
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 36
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 130
8.9

Otherwise Unclassified Properties

Base Metal Price, % relative 19
7.0
Density, g/cm3 2.6
8.0
Embodied Carbon, kg CO2/kg material 8.7
2.5
Embodied Energy, MJ/kg 160
36
Embodied Water, L/kg 1090
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 12 to 20
120
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 710
550
Stiffness to Weight: Axial, points 15
13
Stiffness to Weight: Bending, points 53
24
Strength to Weight: Axial, points 37 to 39
20
Strength to Weight: Bending, points 42 to 44
19
Thermal Diffusivity, mm2/s 63
11
Thermal Shock Resistance, points 16 to 17
17

Alloy Composition


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Aluminum (Al), % 89.1 to 91.8
0 to 0.030
Beryllium (Be), % 0.1 to 0.3
0
Boron (B), % 0
0.0010 to 0.0060
Carbon (C), % 0
0.040 to 0.1
Chromium (Cr), % 0 to 0.2
1.9 to 2.6
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.3
93.2 to 96.2
Magnesium (Mg), % 0.4 to 0.6
0
Manganese (Mn), % 0 to 0.2
0.1 to 0.6
Molybdenum (Mo), % 0
0.050 to 0.3
Nickel (Ni), % 0
0 to 0.4
Niobium (Nb), % 0
0.020 to 0.080
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 7.6 to 8.6
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0.1 to 0.2
0.0050 to 0.060
Tungsten (W), % 0
1.5 to 1.8
Vanadium (V), % 0
0.2 to 0.3
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0