Aerospace Materials: 2024 BAR T851
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) | Fbru ksi (ksi) | Fbru ksi 2 (ksi) | Fcy ksi (ksi) | Ftu ksi (ksi) | Fty ksi LT (ksi) | G Msi (Msi) | basis | condition | density lb in3 (lb/in^3) | elongation pct (%) | form | poisson ratio | specification |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2024 BAR T851 ANY S | 70 | 10.5 | 10.7 | 5 | 58 | 46 | 50 | 5 | 4 | S | T851 | 0.1 | 5 | Bar and rod; rolled, drawn, or cold finished . . . . . . . . . . . . . . . . . . . | 0.33 | AMS-QQ-A-225/6 . . . . . . . . . . . . . . . . . . . |
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