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SAE-AISI D2 Steel vs. 5026 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 5026 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 5026 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
70
Elongation at Break, % 5.0 to 16
5.1 to 11
Fatigue Strength, MPa 310 to 860
94 to 140
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 460 to 1160
150 to 180
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
260 to 320
Tensile Strength: Yield (Proof), MPa 470 to 1510
120 to 250

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Melting Completion (Liquidus), °C 1440
650
Melting Onset (Solidus), °C 1390
510
Specific Heat Capacity, J/kg-K 480
890
Thermal Conductivity, W/m-K 31
130
Thermal Expansion, µm/m-K 11
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
31
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
99

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
9.5
Density, g/cm3 7.7
2.8
Embodied Carbon, kg CO2/kg material 3.4
8.9
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
15 to 29
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
100 to 440
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
49
Strength to Weight: Axial, points 27 to 72
26 to 32
Strength to Weight: Bending, points 24 to 46
33 to 37
Thermal Diffusivity, mm2/s 8.3
52
Thermal Shock Resistance, points 25 to 67
11 to 14

Alloy Composition

Aluminum (Al), % 0
88.2 to 94.7
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0 to 0.3
Copper (Cu), % 0 to 0.25
0.1 to 0.8
Iron (Fe), % 81.3 to 86.9
0.2 to 1.0
Magnesium (Mg), % 0
3.9 to 4.9
Manganese (Mn), % 0 to 0.6
0.6 to 1.8
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
0.55 to 1.4
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.2
Vanadium (V), % 0 to 1.1
0
Zinc (Zn), % 0
0 to 1.0
Zirconium (Zr), % 0
0 to 0.3
Residuals, % 0
0 to 0.15

Comparable Variants