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Annealed ASTM F15 vs. Annealed SAE-AISI H19

Both annealed ASTM F15 and annealed SAE-AISI H19 are iron alloys. Both are furnished in the annealed condition. They have 58% 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 H19.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 160
220
Elastic (Young's, Tensile) Modulus, GPa 190
190
Poisson's Ratio 0.3
0.29
Shear Modulus, GPa 73
75
Tensile Strength: Ultimate (UTS), MPa 520
720

Thermal Properties

Latent Heat of Fusion, J/g 270
260
Melting Completion (Liquidus), °C 1410
1540
Melting Onset (Solidus), °C 1450
1490
Specific Heat Capacity, J/kg-K 460
460
Thermal Conductivity, W/m-K 17
29
Thermal Expansion, µm/m-K 6.0
12

Otherwise Unclassified Properties

Base Metal Price, % relative 49
22
Density, g/cm3 8.3
8.2
Embodied Carbon, kg CO2/kg material 5.2
7.5
Embodied Energy, MJ/kg 71
110
Embodied Water, L/kg 190
110

Common Calculations

Stiffness to Weight: Axial, points 13
13
Stiffness to Weight: Bending, points 23
24
Strength to Weight: Axial, points 17
24
Strength to Weight: Bending, points 17
22
Thermal Diffusivity, mm2/s 4.5
7.9
Thermal Shock Resistance, points 32
21

Alloy Composition

Aluminum (Al), % 0 to 0.1
0
Carbon (C), % 0 to 0.040
0.32 to 0.45
Chromium (Cr), % 0 to 0.2
4.0 to 4.8
Cobalt (Co), % 16 to 18
4.0 to 4.5
Copper (Cu), % 0 to 0.2
0 to 0.25
Iron (Fe), % 50.3 to 56
81.4 to 85.5
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
0.2 to 0.5
Molybdenum (Mo), % 0 to 0.2
0.3 to 0.55
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 0.5
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.1
0
Tungsten (W), % 0
3.8 to 4.5
Vanadium (V), % 0
1.8 to 2.2
Zirconium (Zr), % 0 to 0.1
0