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SAE-AISI D2 Steel vs. 7049A Aluminum

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

Metric UnitsUS Customary Units

Mechanical Properties

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

Thermal Properties

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

Electrical Properties

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

Otherwise Unclassified Properties

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

Common Calculations

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

Alloy Composition

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