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295.0 Aluminum vs. N08320 Stainless Steel

295.0 aluminum belongs to the aluminum alloys classification, while N08320 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 295.0 aluminum and the bottom bar is N08320 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60 to 93
190
Elastic (Young's, Tensile) Modulus, GPa 71
200
Elongation at Break, % 2.0 to 7.2
40
Fatigue Strength, MPa 44 to 55
190
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
78
Shear Strength, MPa 180 to 230
400
Tensile Strength: Ultimate (UTS), MPa 230 to 280
580
Tensile Strength: Yield (Proof), MPa 100 to 220
220

Thermal Properties

Latent Heat of Fusion, J/g 400
300
Maximum Temperature: Mechanical, °C 170
1100
Melting Completion (Liquidus), °C 640
1400
Melting Onset (Solidus), °C 530
1350
Specific Heat Capacity, J/kg-K 880
480
Thermal Conductivity, W/m-K 140
12
Thermal Expansion, µm/m-K 23
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 35
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 100
2.0

Otherwise Unclassified Properties

Base Metal Price, % relative 10
28
Density, g/cm3 3.0
8.0
Embodied Carbon, kg CO2/kg material 7.9
4.9
Embodied Energy, MJ/kg 150
69
Embodied Water, L/kg 1140
200

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 5.2 to 13
180
Resilience: Unit (Modulus of Resilience), kJ/m3 77 to 340
120
Stiffness to Weight: Axial, points 13
14
Stiffness to Weight: Bending, points 46
24
Strength to Weight: Axial, points 21 to 26
20
Strength to Weight: Bending, points 27 to 32
20
Thermal Diffusivity, mm2/s 54
3.3
Thermal Shock Resistance, points 9.8 to 12
13

Alloy Composition

Aluminum (Al), % 91.4 to 95.3
0
Carbon (C), % 0
0 to 0.050
Chromium (Cr), % 0
21 to 23
Copper (Cu), % 4.0 to 5.0
0
Iron (Fe), % 0 to 1.0
40.4 to 50
Magnesium (Mg), % 0 to 0.030
0
Manganese (Mn), % 0 to 0.35
0 to 2.5
Nickel (Ni), % 0
25 to 27
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 0.7 to 1.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 0.35
0
Residuals, % 0 to 0.15
0