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SAE-AISI D2 Steel vs. 2219 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 2219 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 2219 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
72
Elongation at Break, % 5.0 to 16
2.2 to 20
Fatigue Strength, MPa 310 to 860
90 to 130
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 460 to 1160
110 to 280
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
180 to 480
Tensile Strength: Yield (Proof), MPa 470 to 1510
88 to 390

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
110 to 170
Thermal Expansion, µm/m-K 11
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
28 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
81 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
8.2
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
9.6 to 60
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
54 to 1060
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
44
Strength to Weight: Axial, points 27 to 72
16 to 43
Strength to Weight: Bending, points 24 to 46
23 to 44
Thermal Diffusivity, mm2/s 8.3
42 to 63
Thermal Shock Resistance, points 25 to 67
8.2 to 22

Alloy Composition

Aluminum (Al), % 0
91.5 to 93.8
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0
Copper (Cu), % 0 to 0.25
5.8 to 6.8
Iron (Fe), % 81.3 to 86.9
0 to 0.3
Magnesium (Mg), % 0
0 to 0.020
Manganese (Mn), % 0 to 0.6
0.2 to 0.4
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 0.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0.020 to 0.1
Vanadium (V), % 0 to 1.1
0.050 to 0.15
Zinc (Zn), % 0
0 to 0.1
Zirconium (Zr), % 0
0.1 to 0.25
Residuals, % 0
0 to 0.15

Comparable Variants