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SAE-AISI 4340 Steel vs. 514.0 Aluminum

SAE-AISI 4340 steel belongs to the iron alloys classification, while 514.0 aluminum belongs to the aluminum alloys. There are 31 material properties with values for both materials. Properties with values for just one material (1, 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 4340 steel and the bottom bar is 514.0 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210 to 360
50
Elastic (Young's, Tensile) Modulus, GPa 190
68
Elongation at Break, % 12 to 22
7.3
Fatigue Strength, MPa 330 to 740
48
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 73
25
Shear Strength, MPa 430 to 770
140
Tensile Strength: Ultimate (UTS), MPa 690 to 1280
180
Tensile Strength: Yield (Proof), MPa 470 to 1150
74

Thermal Properties

Latent Heat of Fusion, J/g 250
400
Maximum Temperature: Mechanical, °C 430
170
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
610
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 44
140
Thermal Expansion, µm/m-K 13
24

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.5
35
Electrical Conductivity: Equal Weight (Specific), % IACS 8.6
120

Otherwise Unclassified Properties

Base Metal Price, % relative 3.5
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.7
8.9
Embodied Energy, MJ/kg 22
150
Embodied Water, L/kg 53
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 79 to 170
11
Resilience: Unit (Modulus of Resilience), kJ/m3 590 to 3490
41
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 24
51
Strength to Weight: Axial, points 24 to 45
19
Strength to Weight: Bending, points 22 to 33
26
Thermal Diffusivity, mm2/s 12
57
Thermal Shock Resistance, points 20 to 38
7.9

Alloy Composition

Aluminum (Al), % 0
93.6 to 96.5
Carbon (C), % 0.38 to 0.43
0
Chromium (Cr), % 0.7 to 0.9
0
Copper (Cu), % 0
0 to 0.15
Iron (Fe), % 95.1 to 96.3
0 to 0.5
Magnesium (Mg), % 0
3.5 to 4.5
Manganese (Mn), % 0.6 to 0.8
0 to 0.35
Molybdenum (Mo), % 0.2 to 0.3
0
Nickel (Ni), % 1.7 to 2.0
0
Phosphorus (P), % 0 to 0.035
0
Silicon (Si), % 0.15 to 0.35
0 to 0.35
Sulfur (S), % 0 to 0.040
0
Titanium (Ti), % 0
0 to 0.25
Zinc (Zn), % 0
0 to 0.15
Residuals, % 0
0 to 0.15