5019 Aluminum vs. ACI-ASTM CB7Cu-1 Steel
5019 aluminum belongs to the aluminum alloys classification, while ACI-ASTM CB7Cu-1 steel belongs to the iron alloys. There are 28 material properties with values for both materials. Properties with values for just one material (5, 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 5019 aluminum and the bottom bar is ACI-ASTM CB7Cu-1 steel.
Metric UnitsUS Customary Units
Mechanical Properties
Elastic (Young's, Tensile) Modulus, GPa | 68 | |
190 |
Elongation at Break, % | 2.2 to 18 | |
5.7 to 11 |
Fatigue Strength, MPa | 100 to 160 | |
420 to 590 |
Poisson's Ratio | 0.33 | |
0.28 |
Shear Modulus, GPa | 26 | |
76 |
Tensile Strength: Ultimate (UTS), MPa | 280 to 360 | |
960 to 1350 |
Tensile Strength: Yield (Proof), MPa | 120 to 300 | |
760 to 1180 |
Thermal Properties
Latent Heat of Fusion, J/g | 400 | |
280 |
Melting Completion (Liquidus), °C | 640 | |
1430 |
Melting Onset (Solidus), °C | 540 | |
1500 |
Specific Heat Capacity, J/kg-K | 900 | |
480 |
Thermal Conductivity, W/m-K | 130 | |
17 |
Thermal Expansion, µm/m-K | 24 | |
11 |
Electrical Properties
Electrical Conductivity: Equal Volume, % IACS | 29 | |
2.0 |
Electrical Conductivity: Equal Weight (Specific), % IACS | 98 | |
2.3 |
Otherwise Unclassified Properties
Base Metal Price, % relative | 9.5 | |
13 |
Density, g/cm3 | 2.7 | |
7.8 |
Embodied Carbon, kg CO2/kg material | 9.0 | |
2.6 |
Embodied Energy, MJ/kg | 150 | |
38 |
Embodied Water, L/kg | 1180 | |
130 |
Common Calculations
Resilience: Ultimate (Unit Rupture Work), MJ/m3 | 7.6 to 40 | |
71 to 120 |
Resilience: Unit (Modulus of Resilience), kJ/m3 | 110 to 650 | |
1500 to 3590 |
Stiffness to Weight: Axial, points | 14 | |
14 |
Stiffness to Weight: Bending, points | 51 | |
25 |
Strength to Weight: Axial, points | 29 to 38 | |
34 to 48 |
Strength to Weight: Bending, points | 35 to 42 | |
28 to 35 |
Thermal Diffusivity, mm2/s | 52 | |
4.6 |
Thermal Shock Resistance, points | 13 to 16 | |
32 to 45 |
Alloy Composition
Aluminum (Al), % | 91.5 to 95.3 | |
0 |
Carbon (C), % | 0 | |
0 to 0.070 |
Chromium (Cr), % | 0 to 0.2 | |
15.5 to 17.7 |
Copper (Cu), % | 0 to 0.1 | |
2.5 to 3.2 |
Iron (Fe), % | 0 to 0.5 | |
72.3 to 78.4 |
Magnesium (Mg), % | 4.5 to 5.6 | |
0 |
Manganese (Mn), % | 0.1 to 0.6 | |
0 to 0.7 |
Nickel (Ni), % | 0 | |
3.6 to 4.6 |
Niobium (Nb), % | 0 | |
0 to 0.35 |
Nitrogen (N), % | 0 | |
0 to 0.050 |
Phosphorus (P), % | 0 | |
0 to 0.035 |
Silicon (Si), % | 0 to 0.4 | |
0 to 1.0 |
Sulfur (S), % | 0 | |
0 to 0.030 |
Titanium (Ti), % | 0 to 0.2 | |
0 |
Zinc (Zn), % | 0 to 0.2 | |
0 |
Residuals, % | 0 to 0.15 | |
0 |