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713.0 Aluminum vs. S44536 Stainless Steel

713.0 aluminum belongs to the aluminum alloys classification, while S44536 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 S44536 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 74 to 75
170
Elastic (Young's, Tensile) Modulus, GPa 71
200
Elongation at Break, % 3.9 to 4.3
22
Fatigue Strength, MPa 63 to 120
190
Poisson's Ratio 0.32
0.27
Shear Modulus, GPa 27
78
Shear Strength, MPa 180
290
Tensile Strength: Ultimate (UTS), MPa 240 to 260
460
Tensile Strength: Yield (Proof), MPa 170
280

Thermal Properties

Latent Heat of Fusion, J/g 370
290
Maximum Temperature: Mechanical, °C 180
990
Melting Completion (Liquidus), °C 630
1440
Melting Onset (Solidus), °C 610
1390
Specific Heat Capacity, J/kg-K 860
480
Thermal Conductivity, W/m-K 150
21
Thermal Expansion, µm/m-K 24
11

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
2.6
Electrical Conductivity: Equal Weight (Specific), % IACS 100
3.0

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
13
Density, g/cm3 3.1
7.7
Embodied Carbon, kg CO2/kg material 7.8
2.8
Embodied Energy, MJ/kg 150
41
Embodied Water, L/kg 1110
140

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 8.7 to 9.9
89
Resilience: Unit (Modulus of Resilience), kJ/m3 210 to 220
200
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
5.6
Thermal Shock Resistance, points 10 to 11
16

Alloy Composition

Aluminum (Al), % 87.6 to 92.4
0
Carbon (C), % 0
0 to 0.015
Chromium (Cr), % 0 to 0.35
20 to 23
Copper (Cu), % 0.4 to 1.0
0
Iron (Fe), % 0 to 1.1
72.8 to 80
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 to 0.5
Niobium (Nb), % 0
0.050 to 0.8
Nitrogen (N), % 0
0 to 0.015
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0 to 0.25
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0 to 0.8
Zinc (Zn), % 7.0 to 8.0
0
Residuals, % 0 to 0.25
0