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7049A Aluminum vs. SAE-AISI D2 Steel

7049A aluminum belongs to the aluminum alloys classification, while SAE-AISI D2 steel belongs to the iron alloys. There are 29 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 7049A aluminum and the bottom bar is SAE-AISI D2 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 5.0 to 5.7
5.0 to 16
Fatigue Strength, MPa 180
310 to 860
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 27
75
Shear Strength, MPa 340 to 350
460 to 1160
Tensile Strength: Ultimate (UTS), MPa 580 to 590
760 to 2000
Tensile Strength: Yield (Proof), MPa 500 to 530
470 to 1510

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Melting Completion (Liquidus), °C 640
1440
Melting Onset (Solidus), °C 430
1390
Specific Heat Capacity, J/kg-K 850
480
Thermal Conductivity, W/m-K 130
31
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 40
4.3
Electrical Conductivity: Equal Weight (Specific), % IACS 120
5.1

Otherwise Unclassified Properties

Base Metal Price, % relative 10
8.0
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 8.2
3.4
Embodied Energy, MJ/kg 150
50
Embodied Water, L/kg 1100
100

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 28 to 32
92 to 100
Resilience: Unit (Modulus of Resilience), kJ/m3 1800 to 1990
570 to 5940
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 44
25
Strength to Weight: Axial, points 52 to 53
27 to 72
Strength to Weight: Bending, points 50 to 51
24 to 46
Thermal Diffusivity, mm2/s 50
8.3
Thermal Shock Resistance, points 25
25 to 67

Alloy Composition

Aluminum (Al), % 84.6 to 89.5
0
Carbon (C), % 0
1.4 to 1.6
Chromium (Cr), % 0.050 to 0.25
11 to 13
Copper (Cu), % 1.2 to 1.9
0 to 0.25
Iron (Fe), % 0 to 0.5
81.3 to 86.9
Magnesium (Mg), % 2.1 to 3.1
0
Manganese (Mn), % 0 to 0.5
0 to 0.6
Molybdenum (Mo), % 0
0.7 to 1.2
Nickel (Ni), % 0
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.4
0 to 0.6
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0 to 1.1
Zinc (Zn), % 7.2 to 8.4
0
Zirconium (Zr), % 0 to 0.25
0
Residuals, % 0 to 0.15
0