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5040 Aluminum vs. SAE-AISI 4340M Steel

5040 aluminum belongs to the aluminum alloys classification, while SAE-AISI 4340M steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, 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 5040 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 66 to 74
710
Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 5.7 to 6.8
6.0
Fatigue Strength, MPa 100 to 130
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 140 to 150
1360
Tensile Strength: Ultimate (UTS), MPa 240 to 260
2340
Tensile Strength: Yield (Proof), MPa 190 to 230
1240

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 190
430
Melting Completion (Liquidus), °C 650
1440
Melting Onset (Solidus), °C 600
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 160
38
Thermal Expansion, µm/m-K 23
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 41
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 130
9.1

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
3.9
Density, g/cm3 2.8
7.8
Embodied Carbon, kg CO2/kg material 8.3
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1180
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 14 to 15
120
Resilience: Unit (Modulus of Resilience), kJ/m3 260 to 380
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 24 to 26
84
Strength to Weight: Bending, points 31 to 32
51
Thermal Diffusivity, mm2/s 64
10
Thermal Shock Resistance, points 10 to 11
70

Alloy Composition

Aluminum (Al), % 95.2 to 98
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0.1 to 0.3
0.7 to 1.0
Copper (Cu), % 0 to 0.25
0
Iron (Fe), % 0 to 0.7
93.3 to 94.8
Magnesium (Mg), % 1.0 to 1.5
0
Manganese (Mn), % 0.9 to 1.4
0.65 to 0.9
Molybdenum (Mo), % 0
0.35 to 0.45
Nickel (Ni), % 0
1.7 to 2.0
Phosphorus (P), % 0
0 to 0.012
Silicon (Si), % 0 to 0.3
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.25
0
Residuals, % 0 to 0.15
0