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Annealed ASTM F15 vs. Annealed SAE-AISI T15

Both annealed ASTM F15 and annealed SAE-AISI T15 are iron alloys. Both are furnished in the annealed condition. They have 59% of their average alloy composition in common. There are 22 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 ASTM F15 and the bottom bar is annealed SAE-AISI T15.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
250
Elastic (Young's, Tensile) Modulus, GPa 190
200
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 73
76
Tensile Strength: Ultimate (UTS), MPa 520
830

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1410
1690
Melting Onset (Solidus), °C 1450
1640
Specific Heat Capacity, J/kg-K 460
430
Thermal Conductivity, W/m-K 17
21
Thermal Expansion, µm/m-K 6.0
12

Otherwise Unclassified Properties

Base Metal Price, % relative 49
43
Density, g/cm3 8.3
8.7
Embodied Carbon, kg CO2/kg material 5.2
16
Embodied Energy, MJ/kg 71
250
Embodied Water, L/kg 190
140

Common Calculations

Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
22
Strength to Weight: Axial, points 17
26
Strength to Weight: Bending, points 17
22
Thermal Diffusivity, mm2/s 4.5
5.6
Thermal Shock Resistance, points 32
26

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0 to 0.040
1.5 to 1.6
Chromium (Cr), % 0 to 0.2
3.8 to 5.0
Cobalt (Co), % 16 to 18
4.8 to 5.3
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 50.3 to 56
67.5 to 73.5
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.15 to 0.4
Molybdenum (Mo), % 0 to 0.2
0 to 1.0
Nickel (Ni), % 28 to 30
0 to 0.3
Phosphorus (P), % 0
0 to 0.030
Silicon (Si), % 0 to 0.2
0.15 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
11.8 to 13
Vanadium (V), % 0
4.5 to 5.3
Zirconium (Zr), % 0 to 0.1
0