MakeItFrom.com
Menu (ESC)

328.0 Aluminum vs. EN 1.4859 Stainless Steel

328.0 aluminum belongs to the aluminum alloys classification, while EN 1.4859 stainless steel belongs to the iron alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, 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 328.0 aluminum and the bottom bar is EN 1.4859 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 60 to 82
140
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 1.6 to 2.1
23
Fatigue Strength, MPa 55 to 80
140
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Tensile Strength: Ultimate (UTS), MPa 200 to 270
490
Tensile Strength: Yield (Proof), MPa 120 to 170
210

Thermal Properties

Latent Heat of Fusion, J/g 510
310
Maximum Temperature: Mechanical, °C 180
1050
Melting Completion (Liquidus), °C 620
1410
Melting Onset (Solidus), °C 560
1360
Specific Heat Capacity, J/kg-K 890
470
Thermal Conductivity, W/m-K 120
13
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 30
1.7
Electrical Conductivity: Equal Weight (Specific), % IACS 99
1.9

Otherwise Unclassified Properties

Base Metal Price, % relative 10
36
Density, g/cm3 2.7
8.0
Embodied Carbon, kg CO2/kg material 7.8
6.2
Embodied Energy, MJ/kg 140
88
Embodied Water, L/kg 1070
190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 2.8 to 5.0
91
Resilience: Unit (Modulus of Resilience), kJ/m3 92 to 200
110
Stiffness to Weight: Axial, points 15
14
Stiffness to Weight: Bending, points 51
24
Strength to Weight: Axial, points 21 to 28
17
Strength to Weight: Bending, points 28 to 34
17
Thermal Diffusivity, mm2/s 50
3.4
Thermal Shock Resistance, points 9.2 to 12
11

Alloy Composition

Aluminum (Al), % 84.5 to 91.1
0
Carbon (C), % 0
0.050 to 0.15
Chromium (Cr), % 0 to 0.35
19 to 21
Copper (Cu), % 1.0 to 2.0
0
Iron (Fe), % 0 to 1.0
40.3 to 49
Magnesium (Mg), % 0.2 to 0.6
0
Manganese (Mn), % 0.2 to 0.6
0 to 2.0
Molybdenum (Mo), % 0
0 to 0.5
Nickel (Ni), % 0 to 0.25
31 to 33
Niobium (Nb), % 0
0.5 to 1.5
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 7.5 to 8.5
0.5 to 1.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Zinc (Zn), % 0 to 1.5
0
Residuals, % 0 to 0.5
0