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7049A Aluminum vs. EN 1.7380 Steel

7049A aluminum belongs to the aluminum alloys classification, while EN 1.7380 steel 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 7049A aluminum and the bottom bar is EN 1.7380 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 5.0 to 5.7
19 to 20
Fatigue Strength, MPa 180
200 to 230
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 27
74
Shear Strength, MPa 340 to 350
330 to 350
Tensile Strength: Ultimate (UTS), MPa 580 to 590
540 to 550
Tensile Strength: Yield (Proof), MPa 500 to 530
290 to 330

Thermal Properties

Latent Heat of Fusion, J/g 370
260
Maximum Temperature: Mechanical, °C 200
460
Melting Completion (Liquidus), °C 640
1470
Melting Onset (Solidus), °C 430
1430
Specific Heat Capacity, J/kg-K 850
470
Thermal Conductivity, W/m-K 130
39
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
7.6
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
3.8
Density, g/cm3 3.1
7.9
Embodied Carbon, kg CO2/kg material 8.2
1.8
Embodied Energy, MJ/kg 150
23
Embodied Water, L/kg 1100
59

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 28 to 32
87 to 98
Resilience: Unit (Modulus of Resilience), kJ/m3 1800 to 1990
230 to 280
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 44
24
Strength to Weight: Axial, points 52 to 53
19 to 20
Strength to Weight: Bending, points 50 to 51
19
Thermal Diffusivity, mm2/s 50
11
Thermal Shock Resistance, points 25
15 to 16

Alloy Composition


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Aluminum (Al), % 84.6 to 89.5
0
Carbon (C), % 0
0.080 to 0.14
Chromium (Cr), % 0.050 to 0.25
2.0 to 2.5
Copper (Cu), % 1.2 to 1.9
0 to 0.3
Iron (Fe), % 0 to 0.5
94.6 to 96.6
Magnesium (Mg), % 2.1 to 3.1
0
Manganese (Mn), % 0 to 0.5
0.4 to 0.8
Molybdenum (Mo), % 0
0.9 to 1.1
Nitrogen (N), % 0
0 to 0.012
Phosphorus (P), % 0
0 to 0.020
Silicon (Si), % 0 to 0.4
0 to 0.5
Sulfur (S), % 0
0 to 0.010
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 7.2 to 8.4
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0