Thermal conductivity against densityHigher and further left: spreads more heat for its weightThermal expansion against thermal conductivityLower and further right: warps less when heated
Sources2 documents: Magnesium Elektron, U.S. Department of Defense
Elektron AZ31B Sheet, Plate & Coil (Datasheet 482)Magnesium Elektronarchived copyYield strength: typical, H24, 0.5-6 mm, 0.2 % proof stressUltimate tensile strength: typical, H24, 0.5-6 mmElongation at break: typical, H24, 0.5-6 mm, gauge 5.65√AThermal conductivity: typical (temper/temperature not stated)Thermal expansion: typical (temperature range not stated)Specific heat: typical
2
MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures (2003)U.S. Department of DefenseYoung's modulus (stiffness): typical (handbook physical constant)Density: nominalPoisson's ratio: typical (handbook physical constant)Max service temperature: stated application limit
Magnesium AZ31B-H24 has a thermal conductivity of 76.9 W/m·K (44.4 BTU/hr·ft·°F). Basis: typical (temper/temperature not stated). Source: Magnesium Elektron, Elektron AZ31B Sheet, Plate & Coil (Datasheet 482)archived copy.
Specific heat of Magnesium AZ31B-H24
The specific heat capacity of Magnesium AZ31B-H24 is 1,040 J/kg·K (0.248 BTU/lb·°F). Basis: typical. Source: Magnesium Elektron, Elektron AZ31B Sheet, Plate & Coil (Datasheet 482)archived copy.
Coefficient of thermal expansion of Magnesium AZ31B-H24
Magnesium AZ31B-H24 expands 26.8 µm/m·K (14.9 µin/in·°F): a 100 mm part grows 134 µm over a 50 °C rise. Basis: typical (temperature range not stated). Source: Magnesium Elektron, Elektron AZ31B Sheet, Plate & Coil (Datasheet 482)archived copy.
Thermal diffusivity of Magnesium AZ31B-H24
Computed from the conductivity, density and specific heat (k / ρc): 41.8 mm²/s, how fast a temperature change spreads through it.
Maximum service temperature of Magnesium AZ31B-H24
The maximum service temperature of Magnesium AZ31B-H24 is 149 °C (300 °F). Basis: stated application limit. Source: U.S. Department of Defense, MIL-HDBK-5J, Metallic Materials and Elements for Aerospace Vehicle Structures (2003).