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SAE-AISI D2 Steel vs. 242.0 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 242.0 aluminum belongs to the aluminum alloys. There are 29 material properties with values for both materials. Properties with values for just one material (5, 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 242.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
73
Elongation at Break, % 5.0 to 16
0.5 to 1.5
Fatigue Strength, MPa 310 to 860
55 to 110
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
27
Shear Strength, MPa 460 to 1160
150 to 240
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
180 to 290
Tensile Strength: Yield (Proof), MPa 470 to 1510
120 to 220

Thermal Properties

Latent Heat of Fusion, J/g 270
390
Melting Completion (Liquidus), °C 1440
640
Melting Onset (Solidus), °C 1390
530
Specific Heat Capacity, J/kg-K 480
870
Thermal Conductivity, W/m-K 31
130 to 170
Thermal Expansion, µm/m-K 11
22

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
33 to 44
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
96 to 130

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
12
Density, g/cm3 7.7
3.1
Embodied Carbon, kg CO2/kg material 3.4
8.3
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1130

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
1.3 to 3.4
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
110 to 340
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 25
45
Strength to Weight: Axial, points 27 to 72
16 to 26
Strength to Weight: Bending, points 24 to 46
23 to 32
Thermal Diffusivity, mm2/s 8.3
50 to 62
Thermal Shock Resistance, points 25 to 67
8.0 to 13

Alloy Composition

Aluminum (Al), % 0
88.4 to 93.6
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0 to 0.25
Copper (Cu), % 0 to 0.25
3.5 to 4.5
Iron (Fe), % 81.3 to 86.9
0 to 1.0
Magnesium (Mg), % 0
1.2 to 1.8
Manganese (Mn), % 0 to 0.6
0 to 0.35
Molybdenum (Mo), % 0.7 to 1.2
0
Nickel (Ni), % 0 to 0.3
1.7 to 2.3
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0 to 0.6
0 to 0.7
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.25
Vanadium (V), % 0 to 1.1
0
Zinc (Zn), % 0
0 to 0.35
Residuals, % 0
0 to 0.15

Comparable Variants