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Aerospace Materials: MG-AZ31B PLATE H24

Aerospace material mechanical properties and design allowables at ambient, elevated, and cryogenic temperatures per MMPDS-11 (Metallic Materials Properties Development and Standardization). Covers primary structural alloys: aluminum (2024-T3, 7075-T6, 6061-T6, 2219-T87), titanium (Ti-6Al-4V), nickel superalloys (Inconel 718), and steels (300M, 4130, 4340).

Materials Sciencematerial id: MG-AZ31B PLATE H245 rows
material idtemp fE Msi (Msi)Ec Msi (Msi)Fbru ksi (ksi)Fbru ksi 2 (ksi)Fbry ksi (ksi)Fbry ksi 2 (ksi)Fcy ksi (ksi)Fsu ksi (ksi)Ftu ksi (ksi)Ftu ksi LT (ksi)Fty ksi (ksi)Fty ksi LT (ksi)G Msi (Msi)basisconditiondensity lb in3 (lb/in^3)elongation pct (%)formpoisson ratiospecificationthickness range
MG-AZ31B PLATE H24 0.250-0.374 S706.56.5566538382018383926292.4SH240.06398Plate0.35AMS 43770.250-0.374
MG-AZ31B PLATE H24 0.375-0.500 S706.56.5546334341618373824272.4SH240.06398Plate0.35AMS 43770.375-0.500
MG-AZ31B PLATE H24 0.501-1.000 S706.56.513363722252.4SH240.06398Plate0.35AMS 43770.501-1.000
MG-AZ31B PLATE H24 1.001-2.000 S706.56.510343520232.4SH240.06398Plate0.35AMS 43771.001-2.000
MG-AZ31B PLATE H24 2.001-3.000 S706.56.5934182.4SH240.06398Plate0.35AMS 43772.001-3.000

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