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Aerospace Materials: MG-AZ31B PLATE H26

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 H267 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 H26 0.250-0.375 S706.56.5586840402218394027302.4SH260.06396Plate0.35AMS 43760.250-0.375
MG-AZ31B PLATE H26 0.376-0.438 S706.56.5566539392118383926292.4SH260.06396Plate0.35AMS 43760.376-0.438
MG-AZ31B PLATE H26 0.439-0.500 S706.56.5566536361818383926292.4SH260.06396Plate0.35AMS 43760.439-0.500
MG-AZ31B PLATE H26 0.501-0.750 S706.56.517373825282.4SH260.06396Plate0.35AMS 43760.501-0.750
MG-AZ31B PLATE H26 0.751-1.000 S706.56.516373823262.4SH260.06396Plate0.35AMS 43760.751-1.000
MG-AZ31B PLATE H26 1.001-1.500 S706.56.515353622252.4SH260.06396Plate0.35AMS 43761.001-1.500
MG-AZ31B PLATE H26 1.501-2.000 S706.56.514353621242.4SH260.06396Plate0.35AMS 43761.501-2.000

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