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ASTM A182 Grade F911 vs. AZ91E Magnesium

ASTM A182 grade F911 belongs to the iron alloys classification, while AZ91E magnesium belongs to the magnesium alloys. There are 31 material properties with values for both materials. Properties with values for just one material (6, 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 AZ91E magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 220
75
Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 20
2.5 to 6.2
Fatigue Strength, MPa 350
81 to 85
Poisson's Ratio 0.28
0.29
Shear Modulus, GPa 76
18
Shear Strength, MPa 430
89 to 150
Tensile Strength: Ultimate (UTS), MPa 690
160 to 260
Tensile Strength: Yield (Proof), MPa 500
96 to 130

Thermal Properties

Latent Heat of Fusion, J/g 270
350
Maximum Temperature: Mechanical, °C 600
130
Melting Completion (Liquidus), °C 1480
600
Melting Onset (Solidus), °C 1440
500
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 26
84
Thermal Expansion, µm/m-K 13
27

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 9.2
10 to 12
Electrical Conductivity: Equal Weight (Specific), % IACS 10
52 to 60

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
22
Embodied Energy, MJ/kg 40
160
Embodied Water, L/kg 90
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 130
3.4 to 12
Resilience: Unit (Modulus of Resilience), kJ/m3 650
100 to 190
Stiffness to Weight: Axial, points 14
15
Stiffness to Weight: Bending, points 24
69
Strength to Weight: Axial, points 24
25 to 42
Strength to Weight: Bending, points 22
37 to 53
Thermal Diffusivity, mm2/s 6.9
49
Thermal Shock Resistance, points 19
9.0 to 15

Alloy Composition

Aluminum (Al), % 0 to 0.020
8.1 to 9.3
Boron (B), % 0.00030 to 0.0060
0
Carbon (C), % 0.090 to 0.13
0
Chromium (Cr), % 8.5 to 9.5
0
Copper (Cu), % 0
0 to 0.015
Iron (Fe), % 86.2 to 88.9
0 to 0.0050
Magnesium (Mg), % 0
88.8 to 91.3
Manganese (Mn), % 0.3 to 0.6
0.17 to 0.35
Molybdenum (Mo), % 0.9 to 1.1
0
Nickel (Ni), % 0 to 0.4
0 to 0.0010
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 0.2
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
0.4 to 1.0
Zirconium (Zr), % 0 to 0.010
0
Residuals, % 0
0 to 0.3