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7049A Aluminum vs. SAE-AISI 51B60 Steel

7049A aluminum belongs to the aluminum alloys classification, while SAE-AISI 51B60 steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 SAE-AISI 51B60 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 5.0 to 5.7
12 to 21
Fatigue Strength, MPa 180
280 to 340
Poisson's Ratio 0.32
0.29
Shear Modulus, GPa 27
73
Shear Strength, MPa 340 to 350
390 to 420
Tensile Strength: Ultimate (UTS), MPa 580 to 590
660
Tensile Strength: Yield (Proof), MPa 500 to 530
400 to 550

Thermal Properties

Latent Heat of Fusion, J/g 370
250
Maximum Temperature: Mechanical, °C 200
420
Melting Completion (Liquidus), °C 640
1450
Melting Onset (Solidus), °C 430
1410
Specific Heat Capacity, J/kg-K 850
470
Thermal Conductivity, W/m-K 130
43
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 120
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
2.1
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 8.2
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1100
49

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 28 to 32
73 to 120
Resilience: Unit (Modulus of Resilience), kJ/m3 1800 to 1990
420 to 800
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 44
24
Strength to Weight: Axial, points 52 to 53
23
Strength to Weight: Bending, points 50 to 51
22
Thermal Diffusivity, mm2/s 50
12
Thermal Shock Resistance, points 25
19

Alloy Composition

Aluminum (Al), % 84.6 to 89.5
0
Boron (B), % 0
0.00050 to 0.0030
Carbon (C), % 0
0.56 to 0.64
Chromium (Cr), % 0.050 to 0.25
0.7 to 0.9
Copper (Cu), % 1.2 to 1.9
0
Iron (Fe), % 0 to 0.5
97 to 97.8
Magnesium (Mg), % 2.1 to 3.1
0
Manganese (Mn), % 0 to 0.5
0.75 to 1.0
Phosphorus (P), % 0
0 to 0.035
Silicon (Si), % 0 to 0.4
0.15 to 0.35
Sulfur (S), % 0
0 to 0.040
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