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Annealed ASTM F15 vs. Annealed SAE-AISI H26

Both annealed ASTM F15 and annealed SAE-AISI H26 are iron alloys. Both are furnished in the annealed condition. They have 54% 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 H26.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
220
Elastic (Young's, Tensile) Modulus, GPa 190
210
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 73
80
Tensile Strength: Ultimate (UTS), MPa 520
720

Thermal Properties

Latent Heat of Fusion, J/g 270
240
Melting Completion (Liquidus), °C 1410
1810
Melting Onset (Solidus), °C 1450
1760
Specific Heat Capacity, J/kg-K 460
410
Thermal Conductivity, W/m-K 17
22
Thermal Expansion, µm/m-K 6.0
12

Otherwise Unclassified Properties

Base Metal Price, % relative 49
45
Density, g/cm3 8.3
9.3
Embodied Carbon, kg CO2/kg material 5.2
8.1
Embodied Energy, MJ/kg 71
120
Embodied Water, L/kg 190
90

Common Calculations

Stiffness to Weight: Axial, points 13
12
Stiffness to Weight: Bending, points 23
21
Strength to Weight: Axial, points 17
22
Strength to Weight: Bending, points 17
19
Thermal Diffusivity, mm2/s 4.5
5.6
Thermal Shock Resistance, points 32
22

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0 to 0.040
0.45 to 0.55
Chromium (Cr), % 0 to 0.2
3.8 to 4.5
Cobalt (Co), % 16 to 18
0
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 50.3 to 56
73.3 to 77.5
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
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
17.3 to 19
Vanadium (V), % 0
0.75 to 1.3
Zirconium (Zr), % 0 to 0.1
0