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Aerospace Materials: 6013 SHEET T6

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: 6013 SHEET T63 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)Fcy ksi LT (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 LT (%)formpoisson ratiospecificationthickness range
6013 SHEET T6 0.010-0.062 S709.910.1851116676484832525247463.8ST60.0988Sheet0.33AMS 4216 and AMS 43470.010-0.062
6013 SHEET T6 0.063-0.125 S709.910.1851116980484832525247463.8ST60.0988Sheet0.33AMS 4216 and AMS 43470.063-0.125
6013 SHEET T6 0.126-0.249 S709.910.1851117182484932525248463.8ST60.0988Sheet0.33AMS 4216 and AMS 43470.126-0.249

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