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EN 1.7366 Steel vs. 1235 Aluminum

EN 1.7366 steel belongs to the iron alloys classification, while 1235 aluminum belongs to the aluminum 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 EN 1.7366 steel and the bottom bar is 1235 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
69
Elongation at Break, % 17 to 19
28 to 34
Fatigue Strength, MPa 160 to 320
23 to 58
Poisson's Ratio 0.29
0.33
Shear Modulus, GPa 74
26
Shear Strength, MPa 290 to 440
52 to 56
Tensile Strength: Ultimate (UTS), MPa 460 to 710
80 to 84
Tensile Strength: Yield (Proof), MPa 230 to 480
23 to 57

Thermal Properties

Latent Heat of Fusion, J/g 260
400
Maximum Temperature: Mechanical, °C 510
170
Melting Completion (Liquidus), °C 1460
640
Melting Onset (Solidus), °C 1420
640
Specific Heat Capacity, J/kg-K 470
900
Thermal Conductivity, W/m-K 40
230
Thermal Expansion, µm/m-K 13
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 8.1
60
Electrical Conductivity: Equal Weight (Specific), % IACS 9.3
200

Otherwise Unclassified Properties

Base Metal Price, % relative 4.3
9.5
Density, g/cm3 7.8
2.7
Embodied Carbon, kg CO2/kg material 1.7
8.3
Embodied Energy, MJ/kg 23
160
Embodied Water, L/kg 69
1190

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 74 to 110
17 to 25
Resilience: Unit (Modulus of Resilience), kJ/m3 140 to 600
3.8 to 24
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 16 to 25
8.2 to 8.6
Strength to Weight: Bending, points 17 to 23
15 to 16
Thermal Diffusivity, mm2/s 11
93
Thermal Shock Resistance, points 13 to 20
3.6 to 3.7

Alloy Composition

Aluminum (Al), % 0
99.35 to 100
Carbon (C), % 0 to 0.18
0
Chromium (Cr), % 4.0 to 6.0
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 91.9 to 95.3
0 to 0.65
Magnesium (Mg), % 0
0 to 0.050
Manganese (Mn), % 0.3 to 0.8
0 to 0.050
Molybdenum (Mo), % 0.45 to 0.65
0
Phosphorus (P), % 0 to 0.025
0
Silicon (Si), % 0 to 0.4
0 to 0.65
Sulfur (S), % 0 to 0.015
0
Titanium (Ti), % 0
0 to 0.060
Vanadium (V), % 0
0 to 0.050
Zinc (Zn), % 0
0 to 0.1