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713.0 Aluminum vs. S41050 Stainless Steel

713.0 aluminum belongs to the aluminum alloys classification, while S41050 stainless 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 713.0 aluminum and the bottom bar is S41050 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 74 to 75
160
Elastic (Young's, Tensile) Modulus, GPa 71
190
Elongation at Break, % 3.9 to 4.3
25
Fatigue Strength, MPa 63 to 120
160
Poisson's Ratio 0.32
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 180
300
Tensile Strength: Ultimate (UTS), MPa 240 to 260
470
Tensile Strength: Yield (Proof), MPa 170
230

Thermal Properties

Latent Heat of Fusion, J/g 370
270
Maximum Temperature: Mechanical, °C 180
720
Melting Completion (Liquidus), °C 630
1440
Melting Onset (Solidus), °C 610
1400
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 150
27
Thermal Expansion, µm/m-K 24
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
7.0
Density, g/cm3 3.1
7.8
Embodied Carbon, kg CO2/kg material 7.8
1.9
Embodied Energy, MJ/kg 150
27
Embodied Water, L/kg 1110
97

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.7 to 9.9
98
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 220
140
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 45
25
Strength to Weight: Axial, points 22 to 23
17
Strength to Weight: Bending, points 28 to 29
17
Thermal Diffusivity, mm2/s 57
7.2
Thermal Shock Resistance, points 10 to 11
17

Alloy Composition

Aluminum (Al), % 87.6 to 92.4
0
Carbon (C), % 0
0 to 0.040
Chromium (Cr), % 0 to 0.35
10.5 to 12.5
Copper (Cu), % 0.4 to 1.0
0
Iron (Fe), % 0 to 1.1
84.2 to 88.9
Magnesium (Mg), % 0.2 to 0.5
0
Manganese (Mn), % 0 to 0.6
0 to 1.0
Nickel (Ni), % 0 to 0.15
0.6 to 1.1
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 7.0 to 8.0
0
Residuals, % 0 to 0.25
0