MakeItFrom.com
Menu (ESC)

ASTM A182 Grade F36 vs. AZ80A Magnesium

ASTM A182 grade F36 belongs to the iron alloys classification, while AZ80A magnesium belongs to the magnesium alloys. There are 30 material properties with values for both materials. Properties with values for just one material (1, 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 F36 and the bottom bar is AZ80A magnesium.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 190
46
Elongation at Break, % 17
3.9 to 8.5
Fatigue Strength, MPa 330
140 to 170
Poisson's Ratio 0.29
0.29
Shear Modulus, GPa 73
18
Shear Strength, MPa 440
160 to 190
Tensile Strength: Ultimate (UTS), MPa 710
320 to 340
Tensile Strength: Yield (Proof), MPa 490
210 to 230

Thermal Properties

Latent Heat of Fusion, J/g 250
350
Maximum Temperature: Mechanical, °C 410
130
Melting Completion (Liquidus), °C 1460
600
Melting Onset (Solidus), °C 1420
490
Specific Heat Capacity, J/kg-K 470
990
Thermal Conductivity, W/m-K 39
77
Thermal Expansion, µm/m-K 13
26

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 7.6
11
Electrical Conductivity: Equal Weight (Specific), % IACS 8.6
59

Otherwise Unclassified Properties

Base Metal Price, % relative 3.4
12
Density, g/cm3 7.9
1.7
Embodied Carbon, kg CO2/kg material 1.7
23
Embodied Energy, MJ/kg 22
160
Embodied Water, L/kg 53
990

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 110
12 to 24
Resilience: Unit (Modulus of Resilience), kJ/m3 650
500 to 600
Stiffness to Weight: Axial, points 13
15
Stiffness to Weight: Bending, points 24
69
Strength to Weight: Axial, points 25
51 to 55
Strength to Weight: Bending, points 22
60 to 63
Thermal Diffusivity, mm2/s 10
45
Thermal Shock Resistance, points 21
19 to 20

Alloy Composition

Aluminum (Al), % 0 to 0.050
7.8 to 9.2
Carbon (C), % 0.1 to 0.17
0
Chromium (Cr), % 0 to 0.3
0
Copper (Cu), % 0.5 to 0.8
0 to 0.050
Iron (Fe), % 95 to 97.1
0 to 0.0050
Magnesium (Mg), % 0
89 to 91.9
Manganese (Mn), % 0.8 to 1.2
0.12 to 0.5
Molybdenum (Mo), % 0.25 to 0.5
0
Nickel (Ni), % 1.0 to 1.3
0 to 0.0050
Niobium (Nb), % 0.015 to 0.045
0
Nitrogen (N), % 0 to 0.020
0
Phosphorus (P), % 0 to 0.030
0
Silicon (Si), % 0.25 to 0.5
0 to 0.1
Sulfur (S), % 0 to 0.025
0
Vanadium (V), % 0 to 0.020
0
Zinc (Zn), % 0
0.2 to 0.8
Residuals, % 0
0 to 0.3