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Annealed SAE-AISI F1 vs. Annealed SAE-AISI T8

Both annealed SAE-AISI F1 and annealed SAE-AISI T8 are iron alloys. Both are furnished in the annealed condition. They have 75% of their average alloy composition in common. There are 23 material properties with values for both materials. Properties with values for just one material (9, in this case) are not shown.

For each property being compared, the top bar is annealed SAE-AISI F1 and the bottom bar is annealed SAE-AISI T8.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 190
240
Elastic (Young's, Tensile) Modulus, GPa 190
200
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 72
78
Tensile Strength: Ultimate (UTS), MPa 620
780

Thermal Properties

Latent Heat of Fusion, J/g 250
250
Melting Completion (Liquidus), °C 1480
1730
Melting Onset (Solidus), °C 1430
1670
Specific Heat Capacity, J/kg-K 470
420
Thermal Conductivity, W/m-K 45
18
Thermal Expansion, µm/m-K 13
12

Otherwise Unclassified Properties

Base Metal Price, % relative 5.0
45
Density, g/cm3 7.9
9.0
Embodied Carbon, kg CO2/kg material 1.7
10
Embodied Energy, MJ/kg 24
160
Embodied Water, L/kg 46
120

Common Calculations

PREN (Pitting Resistance) 2.3
30
Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 24
22
Strength to Weight: Axial, points 22
24
Strength to Weight: Bending, points 20
21
Thermal Diffusivity, mm2/s 12
4.8
Thermal Shock Resistance, points 19
24

Alloy Composition

Carbon (C), % 1.0 to 1.3
0.75 to 0.85
Chromium (Cr), % 0
3.8 to 4.5
Cobalt (Co), % 0
4.3 to 5.8
Copper (Cu), % 0
0 to 0.25
Iron (Fe), % 95.9 to 98
69.3 to 75.4
Manganese (Mn), % 0 to 0.5
0.2 to 0.4
Molybdenum (Mo), % 0
0.4 to 1.0
Nickel (Ni), % 0
0 to 0.3
Phosphorus (P), % 0 to 0.030
0 to 0.030
Silicon (Si), % 0.1 to 0.5
0.2 to 0.4
Sulfur (S), % 0 to 0.030
0 to 0.030
Tungsten (W), % 1.0 to 1.8
13.3 to 14.8
Vanadium (V), % 0
1.8 to 2.4