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Sintered 2014 Aluminum vs. EN 1.0038 Steel

Sintered 2014 aluminum belongs to the aluminum alloys classification, while EN 1.0038 steel belongs to the iron alloys. There are 29 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 sintered 2014 aluminum and the bottom bar is EN 1.0038 steel.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 70
190
Elongation at Break, % 0.5 to 3.0
23 to 25
Fatigue Strength, MPa 52 to 100
140 to 160
Poisson's Ratio 0.33
0.29
Shear Modulus, GPa 26
73
Tensile Strength: Ultimate (UTS), MPa 140 to 290
380 to 430
Tensile Strength: Yield (Proof), MPa 97 to 280
200 to 220

Thermal Properties

Latent Heat of Fusion, J/g 390
250
Maximum Temperature: Mechanical, °C 170
400
Melting Completion (Liquidus), °C 650
1460
Melting Onset (Solidus), °C 560
1420
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 130
49
Thermal Expansion, µm/m-K 23
12

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 33
7.2
Electrical Conductivity: Equal Weight (Specific), % IACS 100
8.3

Otherwise Unclassified Properties

Base Metal Price, % relative 10
2.1
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 8.0
1.4
Embodied Energy, MJ/kg 150
19
Embodied Water, L/kg 1150
48

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 1.0 to 5.7
72 to 88
Resilience: Unit (Modulus of Resilience), kJ/m3 68 to 560
110 to 130
Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 47
24
Strength to Weight: Axial, points 13 to 27
13 to 15
Strength to Weight: Bending, points 20 to 33
15 to 16
Thermal Diffusivity, mm2/s 51
13
Thermal Shock Resistance, points 6.2 to 13
12 to 13

Alloy Composition

Aluminum (Al), % 91.5 to 96.3
0
Carbon (C), % 0
0 to 0.23
Chromium (Cr), % 0
0 to 0.3
Copper (Cu), % 3.5 to 5.0
0 to 0.6
Iron (Fe), % 0
97.1 to 100
Magnesium (Mg), % 0.2 to 0.8
0
Manganese (Mn), % 0
0 to 1.5
Molybdenum (Mo), % 0
0 to 0.080
Nickel (Ni), % 0
0 to 0.3
Nitrogen (N), % 0
0 to 0.014
Phosphorus (P), % 0
0 to 0.045
Silicon (Si), % 0 to 1.2
0 to 0.55
Sulfur (S), % 0
0 to 0.045
Residuals, % 0 to 1.5
0