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Hot Rolled SAE-AISI 1049 vs. Hot Worked Nickel 201

Hot rolled SAE-AISI 1049 belongs to the iron alloys classification, while hot worked nickel 201 belongs to the nickel 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.

For each property being compared, the top bar is hot rolled SAE-AISI 1049 and the bottom bar is hot worked nickel 201.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
180
Elongation at Break, % 17
45
Fatigue Strength, MPa 250
68
Poisson's Ratio 0.29
0.31
Shear Modulus, GPa 72
70
Shear Strength, MPa 420
270
Tensile Strength: Ultimate (UTS), MPa 680
390
Tensile Strength: Yield (Proof), MPa 370
80

Thermal Properties

Latent Heat of Fusion, J/g 250
290
Maximum Temperature: Mechanical, °C 400
900
Melting Completion (Liquidus), °C 1460
1450
Melting Onset (Solidus), °C 1420
1440
Specific Heat Capacity, J/kg-K 470
440
Thermal Conductivity, W/m-K 51
78
Thermal Expansion, µm/m-K 12
13

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.0
19
Electrical Conductivity: Equal Weight (Specific), % IACS 8.1
19

Otherwise Unclassified Properties

Base Metal Price, % relative 1.8
65
Density, g/cm3 7.8
8.9
Embodied Carbon, kg CO2/kg material 1.4
11
Embodied Energy, MJ/kg 18
150
Embodied Water, L/kg 46
230

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 99
130
Resilience: Unit (Modulus of Resilience), kJ/m3 370
17
Stiffness to Weight: Axial, points 13
11
Stiffness to Weight: Bending, points 24
21
Strength to Weight: Axial, points 24
12
Strength to Weight: Bending, points 22
13
Thermal Diffusivity, mm2/s 14
20
Thermal Shock Resistance, points 22
11

Alloy Composition

Carbon (C), % 0.46 to 0.53
0 to 0.020
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 98.5 to 98.9
0 to 0.4
Manganese (Mn), % 0.6 to 0.9
0 to 0.35
Nickel (Ni), % 0
99 to 100
Phosphorus (P), % 0 to 0.040
0
Silicon (Si), % 0
0 to 0.35
Sulfur (S), % 0 to 0.050
0 to 0.010