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5657 Aluminum vs. SAE-AISI 4340M Steel

5657 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 5657 aluminum and the bottom bar is SAE-AISI 4340M steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 40 to 50
710
Elastic (Young's, Tensile) Modulus, GPa 68
190
Elongation at Break, % 6.6 to 15
6.0
Fatigue Strength, MPa 74 to 88
690
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
72
Shear Strength, MPa 92 to 110
1360
Tensile Strength: Ultimate (UTS), MPa 150 to 200
2340
Tensile Strength: Yield (Proof), MPa 140 to 170
1240

Thermal Properties

Latent Heat of Fusion, J/g 400
280
Maximum Temperature: Mechanical, °C 180
430
Melting Completion (Liquidus), °C 660
1440
Melting Onset (Solidus), °C 640
1400
Specific Heat Capacity, J/kg-K 900
480
Thermal Conductivity, W/m-K 210
38
Thermal Expansion, µm/m-K 24
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 54
7.8
Electrical Conductivity: Equal Weight (Specific), % IACS 180
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 8.4
1.9
Embodied Energy, MJ/kg 160
26
Embodied Water, L/kg 1200
55

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 9.7 to 27
120
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 200
4120
Stiffness to Weight: Axial, points 14
13
Stiffness to Weight: Bending, points 50
25
Strength to Weight: Axial, points 15 to 20
84
Strength to Weight: Bending, points 23 to 28
51
Thermal Diffusivity, mm2/s 84
10
Thermal Shock Resistance, points 6.7 to 8.6
70

Alloy Composition

Aluminum (Al), % 98.5 to 99.4
0
Carbon (C), % 0
0.38 to 0.43
Chromium (Cr), % 0
0.7 to 1.0
Copper (Cu), % 0 to 0.1
0
Gallium (Ga), % 0 to 0.030
0
Iron (Fe), % 0 to 0.1
93.3 to 94.8
Magnesium (Mg), % 0.6 to 1.0
0
Manganese (Mn), % 0 to 0.030
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 0.080
1.5 to 1.8
Sulfur (S), % 0
0 to 0.012
Vanadium (V), % 0 to 0.050
0.050 to 0.1
Zinc (Zn), % 0 to 0.050
0
Residuals, % 0 to 0.050
0