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5383 Aluminum vs. ASTM A387 Grade 11 Steel

5383 aluminum belongs to the aluminum alloys classification, while ASTM A387 grade 11 steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (2, 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 ASTM A387 grade 11 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 85 to 110
150 to 180
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.7 to 15
25
Fatigue Strength, MPa 130 to 200
200 to 250
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Shear Strength, MPa 190 to 220
320 to 390
Tensile Strength: Ultimate (UTS), MPa 310 to 370
500 to 600
Tensile Strength: Yield (Proof), MPa 150 to 310
270 to 350

Thermal Properties

Latent Heat of Fusion, J/g 390
260
Maximum Temperature: Mechanical, °C 200
430
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 540
1420
Specific Heat Capacity, J/kg-K 900
470
Thermal Conductivity, W/m-K 130
39
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 29
7.4
Electrical Conductivity: Equal Weight (Specific), % IACS 97
8.5

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
2.9
Density, g/cm3 2.7
7.8
Embodied Carbon, kg CO2/kg material 9.0
1.6
Embodied Energy, MJ/kg 160
21
Embodied Water, L/kg 1170
53

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 23 to 40
100 to 130
Resilience: Unit (Modulus of Resilience), kJ/m3 170 to 690
200 to 320
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
24
Strength to Weight: Axial, points 32 to 38
18 to 21
Strength to Weight: Bending, points 38 to 42
18 to 20
Thermal Diffusivity, mm2/s 51
11
Thermal Shock Resistance, points 14 to 16
15 to 18

Alloy Composition

Aluminum (Al), % 92 to 95.3
0
Carbon (C), % 0
0.050 to 0.17
Chromium (Cr), % 0 to 0.25
1.0 to 1.5
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.25
96.2 to 97.6
Magnesium (Mg), % 4.0 to 5.2
0
Manganese (Mn), % 0.7 to 1.0
0.4 to 0.65
Molybdenum (Mo), % 0
0.45 to 0.65
Phosphorus (P), % 0
0 to 0.025
Silicon (Si), % 0 to 0.25
0.5 to 0.8
Sulfur (S), % 0
0 to 0.025
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

Comparable Variants