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SAE-AISI D2 Steel vs. 2011 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 2011 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 2011 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
71
Elongation at Break, % 5.0 to 16
8.5 to 18
Fatigue Strength, MPa 310 to 860
74 to 120
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 460 to 1160
190 to 250
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
310 to 420
Tensile Strength: Yield (Proof), MPa 470 to 1510
140 to 310

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Melting Completion (Liquidus), °C 1440
640
Melting Onset (Solidus), °C 1390
540
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 31
140 to 170
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
35 to 45
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
100 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
11
Density, g/cm3 7.7
3.1
Embodied Carbon, kg CO2/kg material 3.4
7.9
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
29 to 52
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
140 to 680
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
44
Strength to Weight: Axial, points 27 to 72
27 to 37
Strength to Weight: Bending, points 24 to 46
32 to 40
Thermal Diffusivity, mm2/s 8.3
51 to 64
Thermal Shock Resistance, points 25 to 67
14 to 19

Alloy Composition

Aluminum (Al), % 0
91.3 to 94.6
Bismuth (Bi), % 0
0.2 to 0.6
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0
Copper (Cu), % 0 to 0.25
5.0 to 6.0
Iron (Fe), % 81.3 to 86.9
0 to 0.7
Lead (Pb), % 0
0.2 to 0.6
Manganese (Mn), % 0 to 0.6
0
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
Vanadium (V), % 0 to 1.1
0
Zinc (Zn), % 0
0 to 0.3
Residuals, % 0
0 to 0.15