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SAE-AISI D2 Steel vs. 5154 Aluminum

SAE-AISI D2 steel belongs to the iron alloys classification, while 5154 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 5154 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 5.0 to 16
3.4 to 20
Fatigue Strength, MPa 310 to 860
100 to 160
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 75
26
Shear Strength, MPa 460 to 1160
140 to 210
Tensile Strength: Ultimate (UTS), MPa 760 to 2000
240 to 360
Tensile Strength: Yield (Proof), MPa 470 to 1510
94 to 270

Thermal Properties

Latent Heat of Fusion, J/g 270
400
Melting Completion (Liquidus), °C 1440
640
Melting Onset (Solidus), °C 1390
590
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 31
130
Thermal Expansion, µm/m-K 11
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 4.3
32
Electrical Conductivity: Equal Weight (Specific), % IACS 5.1
110

Otherwise Unclassified Properties

Base Metal Price, % relative 8.0
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 3.4
8.8
Embodied Energy, MJ/kg 50
150
Embodied Water, L/kg 100
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 92 to 100
11 to 39
Resilience: Unit (Modulus of Resilience), kJ/m3 570 to 5940
64 to 540
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
51
Strength to Weight: Axial, points 27 to 72
25 to 37
Strength to Weight: Bending, points 24 to 46
32 to 42
Thermal Diffusivity, mm2/s 8.3
52
Thermal Shock Resistance, points 25 to 67
10 to 16

Alloy Composition

Aluminum (Al), % 0
94.4 to 96.8
Carbon (C), % 1.4 to 1.6
0
Chromium (Cr), % 11 to 13
0.15 to 0.35
Copper (Cu), % 0 to 0.25
0 to 0.1
Iron (Fe), % 81.3 to 86.9
0 to 0.4
Magnesium (Mg), % 0
3.1 to 3.9
Manganese (Mn), % 0 to 0.6
0 to 0.1
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 0.25
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 0.2
Residuals, % 0
0 to 0.15

Comparable Variants