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Annealed ASTM F15 vs. Annealed SAE-AISI T6

Both annealed ASTM F15 and annealed SAE-AISI T6 are iron alloys. Both are furnished in the annealed condition. They have 66% 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 T6.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
270
Elastic (Young's, Tensile) Modulus, GPa 190
210
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 73
81
Tensile Strength: Ultimate (UTS), MPa 520
880

Thermal Properties

Latent Heat of Fusion, J/g 270
250
Melting Completion (Liquidus), °C 1410
1830
Melting Onset (Solidus), °C 1450
1770
Specific Heat Capacity, J/kg-K 460
400
Thermal Conductivity, W/m-K 17
18
Thermal Expansion, µm/m-K 6.0
12

Otherwise Unclassified Properties

Base Metal Price, % relative 49
70
Density, g/cm3 8.3
9.5
Embodied Carbon, kg CO2/kg material 5.2
11
Embodied Energy, MJ/kg 71
170
Embodied Water, L/kg 190
160

Common Calculations

Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 23
21
Strength to Weight: Axial, points 17
26
Strength to Weight: Bending, points 17
21
Thermal Diffusivity, mm2/s 4.5
4.7
Thermal Shock Resistance, points 32
26

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0 to 0.040
0.75 to 0.85
Chromium (Cr), % 0 to 0.2
4.0 to 4.8
Cobalt (Co), % 16 to 18
11 to 13
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 50.3 to 56
55.9 to 63.5
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.2 to 0.4
Molybdenum (Mo), % 0 to 0.2
0.4 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
0.2 to 0.4
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
18.5 to 21
Vanadium (V), % 0
1.5 to 2.1
Zirconium (Zr), % 0 to 0.1
0