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ASTM A182 Grade F911 vs. AZ31B Magnesium

ASTM A182 grade F911 belongs to the iron alloys classification, while AZ31B magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is ASTM A182 grade F911 and the bottom bar is AZ31B magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
45
Elongation at Break, % 20
5.6 to 12
Fatigue Strength, MPa 350
100 to 120
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
17
Shear Strength, MPa 430
130 to 160
Tensile Strength: Ultimate (UTS), MPa 690
240 to 270
Tensile Strength: Yield (Proof), MPa 500
120 to 180

Thermal Properties

Latent Heat of Fusion, J/g 270
350
Maximum Temperature: Mechanical, °C 600
150
Melting Completion (Liquidus), °C 1480
600
Melting Onset (Solidus), °C 1440
600
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 26
100
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.2
18
Electrical Conductivity: Equal Weight (Specific), % IACS 10
95

Otherwise Unclassified Properties

Base Metal Price, % relative 9.5
12
Density, g/cm3 7.9
1.7
Embodied Carbon, kg CO2/kg material 2.8
23
Embodied Energy, MJ/kg 40
160
Embodied Water, L/kg 90
970

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
13 to 25
Resilience: Unit (Modulus of Resilience), kJ/m3 650
170 to 370
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 24
70
Strength to Weight: Axial, points 24
39 to 44
Strength to Weight: Bending, points 22
50 to 55
Thermal Diffusivity, mm2/s 6.9
62
Thermal Shock Resistance, points 19
14 to 16

Alloy Composition

Aluminum (Al), % 0 to 0.020
2.4 to 3.6
Boron (B), % 0.00030 to 0.0060
0
Calcium (Ca), % 0
0 to 0.040
Carbon (C), % 0.090 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0
Copper (Cu), % 0
0 to 0.050
Iron (Fe), % 86.2 to 88.9
0 to 0.050
Magnesium (Mg), % 0
93.6 to 97.1
Manganese (Mn), % 0.3 to 0.6
0.050 to 1.0
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.0050
Niobium (Nb), % 0.060 to 0.1
0
Nitrogen (N), % 0.040 to 0.090
0
Phosphorus (P), % 0 to 0.020
0
Silicon (Si), % 0.1 to 0.5
0 to 0.1
Sulfur (S), % 0 to 0.010
0
Titanium (Ti), % 0 to 0.010
0
Tungsten (W), % 0.9 to 1.1
0
Vanadium (V), % 0.18 to 0.25
0
Zinc (Zn), % 0
0.5 to 1.5
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.3