Aerospace Materials: 2014 EXTRUSION 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).
| material id | temp f | E Msi (Msi) | Ec Msi (Msi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2014 EXTRUSION T6 GT 0.750 S | 70 | 10.8 | 11 | 68 | 56 | 58 | 47 | 4.1 | S | T6, T6510, and T6511 | 0.101 | 6 | 1 | Extruded bar, rod, and shapes | 0.33 | AMS 4153 and AMS-QQ-A-200/2 | >=0.750 |
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