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Annealed AISI 205 vs. EN 1.4057 +A Steel

Both annealed AISI 205 and EN 1.4057 +A steel are iron alloys. Both are furnished in the annealed condition. They have 84% of their average alloy composition in common. There are 29 material properties with values for both materials. Properties with values for just one material (6, in this case) are not shown.

For each property being compared, the top bar is annealed AISI 205 and the bottom bar is EN 1.4057 +A steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 210
260
Elastic (Young's, Tensile) Modulus, GPa 200
200
Elongation at Break, % 45
17
Fatigue Strength, MPa 410
320
Poisson's Ratio 0.28
0.28
Shear Modulus, GPa 77
77
Shear Strength, MPa 560
520
Tensile Strength: Ultimate (UTS), MPa 800
840
Tensile Strength: Yield (Proof), MPa 450
530

Thermal Properties

Latent Heat of Fusion, J/g 280
280
Maximum Temperature: Corrosion, °C 410
400
Maximum Temperature: Mechanical, °C 880
850
Melting Completion (Liquidus), °C 1380
1440
Melting Onset (Solidus), °C 1340
1390
Specific Heat Capacity, J/kg-K 480
480
Thermal Expansion, µm/m-K 18
10

Otherwise Unclassified Properties

Base Metal Price, % relative 11
9.5
Density, g/cm3 7.6
7.7
Embodied Carbon, kg CO2/kg material 2.6
2.2
Embodied Energy, MJ/kg 37
32
Embodied Water, L/kg 150
120

Common Calculations

PREN (Pitting Resistance) 23
16
Resilience: Ultimate (Unit Rupture Work), MJ/m3 300
130
Resilience: Unit (Modulus of Resilience), kJ/m3 510
700
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 26
25
Strength to Weight: Axial, points 29
30
Strength to Weight: Bending, points 25
26
Thermal Shock Resistance, points 16
30

Alloy Composition

Carbon (C), % 0.12 to 0.25
0.12 to 0.22
Chromium (Cr), % 16.5 to 18.5
15 to 17
Iron (Fe), % 62.6 to 68.1
77.7 to 83.4
Manganese (Mn), % 14 to 15.5
0 to 1.5
Nickel (Ni), % 1.0 to 1.7
1.5 to 2.5
Nitrogen (N), % 0.32 to 0.4
0
Phosphorus (P), % 0 to 0.060
0 to 0.040
Silicon (Si), % 0 to 1.0
0 to 1.0
Sulfur (S), % 0 to 0.030
0 to 0.015