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5383 Aluminum vs. ACI-ASTM CA15M Steel

5383 aluminum belongs to the aluminum alloys classification, while ACI-ASTM CA15M steel belongs to the iron alloys. There are 31 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 5383 aluminum and the bottom bar is ACI-ASTM CA15M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
210
Elastic (Young's, Tensile) Modulus, GPa 68
200
Elongation at Break, % 6.7 to 15
20
Fatigue Strength, MPa 130 to 200
330
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 26
76
Tensile Strength: Ultimate (UTS), MPa 310 to 370
690
Tensile Strength: Yield (Proof), MPa 150 to 310
510

Thermal Properties

Latent Heat of Fusion, J/g 390
270
Maximum Temperature: Corrosion, °C 65
390
Maximum Temperature: Mechanical, °C 200
760
Melting Completion (Liquidus), °C 650
1450
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 130
27
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
3.0
Electrical Conductivity: Equal Weight (Specific), % IACS 97
3.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.5
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
2.1
Embodied Energy, MJ/kg 160
29
Embodied Water, L/kg 1170
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
130
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
670
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 32 to 38
25
Strength to Weight: Bending, points 38 to 42
22
Thermal Diffusivity, mm2/s 51
7.2
Thermal Shock Resistance, points 14 to 16
25

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0 to 0.15
Chromium (Cr), % 0 to 0.25
11.5 to 14
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
82.1 to 88.4
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0 to 1.0
Molybdenum (Mo), % 0
0.15 to 1.0
Nickel (Ni), % 0
0 to 1.0
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.25
0 to 0.65
Sulfur (S), % 0
0 to 0.040
Titanium (Ti), % 0 to 0.15
0
Zinc (Zn), % 0 to 0.4
0
Zirconium (Zr), % 0 to 0.2
0
Residuals, % 0 to 0.15
0