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Hot Rolled SAE-AISI 1086 vs. Hot Worked Monel 400

Hot rolled SAE-AISI 1086 belongs to the iron alloys classification, while hot worked Monel 400 belongs to the nickel 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.

For each property being compared, the top bar is hot rolled SAE-AISI 1086 and the bottom bar is hot worked Monel 400.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
160
Elongation at Break, % 11
37
Fatigue Strength, MPa 300
290
Poisson's Ratio 0.29
0.32
Shear Modulus, GPa 72
62
Shear Strength, MPa 520
400
Tensile Strength: Ultimate (UTS), MPa 870
600
Tensile Strength: Yield (Proof), MPa 480
260

Thermal Properties

Latent Heat of Fusion, J/g 240
270
Maximum Temperature: Mechanical, °C 400
1000
Melting Completion (Liquidus), °C 1460
1350
Melting Onset (Solidus), °C 1410
1300
Specific Heat Capacity, J/kg-K 470
430
Thermal Conductivity, W/m-K 50
23
Thermal Expansion, µm/m-K 11
14

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
3.3
Electrical Conductivity: Equal Weight (Specific), % IACS 8.1
3.4

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
50
Density, g/cm3 7.8
8.9
Embodied Carbon, kg CO2/kg material 1.4
7.9
Embodied Energy, MJ/kg 19
110
Embodied Water, L/kg 45
250

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 84
180
Resilience: Unit (Modulus of Resilience), kJ/m3 610
210
Stiffness to Weight: Axial, points 13
10
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 31
19
Strength to Weight: Bending, points 26
18
Thermal Diffusivity, mm2/s 14
6.1
Thermal Shock Resistance, points 30
19

Alloy Composition

Carbon (C), % 0.8 to 0.93
0 to 0.3
Copper (Cu), % 0
28 to 34
Iron (Fe), % 98.5 to 98.9
0 to 2.5
Manganese (Mn), % 0.3 to 0.5
0 to 2.0
Nickel (Ni), % 0
63 to 72
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0 to 0.5
Sulfur (S), % 0 to 0.050
0 to 0.024