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SAE-AISI D2 Steel vs. A206.0 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while A206.0 aluminum belongs to the aluminum alloys. There are 29 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 SAE-AISI D2 steel and the bottom bar is A206.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 5.0 to 16
4.2 to 10
Fatigue Strength, MPa 310 to 860
90 to 180
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 460 to 1160
260
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
390 to 440
Tensile Strength: Yield (Proof), MPa 470 to 1510
250 to 380

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Melting Completion (Liquidus), °C 1440
670
Melting Onset (Solidus), °C 1390
550
Specific Heat Capacity, J/kg-K 480
880
Thermal Conductivity, W/m-K 31
130
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
30
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
90

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
11
Density, g/cm3 7.7
3.0
Embodied Carbon, kg CO2/kg material 3.4
8.0
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
16 to 37
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
440 to 1000
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
46
Strength to Weight: Axial, points 27 to 72
36 to 41
Strength to Weight: Bending, points 24 to 46
39 to 43
Thermal Diffusivity, mm2/s 8.3
48
Thermal Shock Resistance, points 25 to 67
17 to 19

Alloy Composition

Aluminum (Al), % 0
93.9 to 95.7
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0
Copper (Cu), % 0 to 0.25
4.2 to 5.0
Iron (Fe), % 81.3 to 86.9
0 to 0.1
Magnesium (Mg), % 0
0 to 0.15
Manganese (Mn), % 0 to 0.6
0 to 0.2
Molybdenum (Mo), % 0.7 to 1.2
0
Nickel (Ni), % 0 to 0.3
0 to 0.050
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.6
0 to 0.050
Sulfur (S), % 0 to 0.030
0
Tin (Sn), % 0
0 to 0.050
Titanium (Ti), % 0
0.15 to 0.3
Vanadium (V), % 0 to 1.1
0
Zinc (Zn), % 0
0 to 0.1
Residuals, % 0
0 to 0.15