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4015 Aluminum vs. SAE-AISI 4340M Steel

4015 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 4015 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 35 to 70
710
Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 1.1 to 23
6.0
Fatigue Strength, MPa 46 to 71
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 82 to 120
1360
Tensile Strength: Ultimate (UTS), MPa 130 to 220
2340
Tensile Strength: Yield (Proof), MPa 50 to 200
1240

Thermal Properties

Latent Heat of Fusion, J/g 420
280
Maximum Temperature: Mechanical, °C 160
430
Melting Completion (Liquidus), °C 640
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 2.7
7.8
Embodied Carbon, kg CO2/kg material 8.1
1.9
Embodied Energy, MJ/kg 150
26
Embodied Water, L/kg 1160
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.4 to 24
120
Resilience: Unit (Modulus of Resilience), kJ/m3 18 to 290
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 13 to 22
84
Strength to Weight: Bending, points 21 to 30
51
Thermal Diffusivity, mm2/s 66
10
Thermal Shock Resistance, points 5.7 to 9.7
70

Alloy Composition

Aluminum (Al), % 94.9 to 97.9
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0
0.7 to 1.0
Copper (Cu), % 0 to 0.2
0
Iron (Fe), % 0 to 0.7
93.3 to 94.8
Magnesium (Mg), % 0.1 to 0.5
0
Manganese (Mn), % 0.6 to 1.2
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), % 1.4 to 2.2
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Vanadium (V), % 0
0.050 to 0.1
Zinc (Zn), % 0 to 0.2
0
Residuals, % 0 to 0.15
0