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296.0 Aluminum vs. S40930 Stainless Steel

296.0 aluminum belongs to the aluminum alloys classification, while S40930 stainless steel belongs to the iron alloys. There are 30 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 296.0 aluminum and the bottom bar is S40930 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 75 to 90
160
Elastic (Young's, Tensile) Modulus, GPa 72
190
Elongation at Break, % 3.2 to 7.1
23
Fatigue Strength, MPa 47 to 70
130
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
75
Tensile Strength: Ultimate (UTS), MPa 260 to 270
430
Tensile Strength: Yield (Proof), MPa 120 to 180
190

Thermal Properties

Latent Heat of Fusion, J/g 420
270
Maximum Temperature: Mechanical, °C 170
710
Melting Completion (Liquidus), °C 630
1450
Melting Onset (Solidus), °C 540
1410
Specific Heat Capacity, J/kg-K 870
480
Thermal Conductivity, W/m-K 130 to 150
25
Thermal Expansion, µm/m-K 22
10

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33 to 37
2.9
Electrical Conductivity: Equal Weight (Specific), % IACS 99 to 110
3.3

Otherwise Unclassified Properties

Base Metal Price, % relative 11
8.5
Density, g/cm3 3.0
7.8
Embodied Carbon, kg CO2/kg material 7.8
2.3
Embodied Energy, MJ/kg 150
32
Embodied Water, L/kg 1110
94

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 7.6 to 15
80
Resilience: Unit (Modulus of Resilience), kJ/m3 110 to 220
94
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
25
Strength to Weight: Axial, points 24 to 25
16
Strength to Weight: Bending, points 30 to 31
16
Thermal Diffusivity, mm2/s 51 to 56
6.7
Thermal Shock Resistance, points 12
16

Alloy Composition

Aluminum (Al), % 89 to 94
0
Carbon (C), % 0
0 to 0.030
Chromium (Cr), % 0
10.5 to 11.7
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.2
84.7 to 89.4
Magnesium (Mg), % 0 to 0.050
0
Manganese (Mn), % 0 to 0.35
0 to 1.0
Nickel (Ni), % 0 to 0.35
0 to 0.5
Niobium (Nb), % 0
0.080 to 0.75
Nitrogen (N), % 0
0 to 0.030
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 2.0 to 3.0
0 to 1.0
Sulfur (S), % 0
0 to 0.020
Titanium (Ti), % 0 to 0.25
0.050 to 0.2
Zinc (Zn), % 0 to 0.5
0
Residuals, % 0 to 0.35
0