Aerospace Materials: 2090 SHEET T83
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) | Fbry ksi (ksi) | Fbry ksi 2 (ksi) | Fcy ksi (ksi) | Fcy ksi LT (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi 45 | 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 |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 2090 SHEET T83 0.040-0.125 S | 70 | 11 | 11.4 | 100 | 126 | 84 | 98 | 67 | 71 | 37 | 77 | 64 | 73 | 70 | 66 | 4.3 | S | T83 | 0.094 | 3 | 5 | Sheet | 0.34 | AMS 4251 | 0.040-0.125 |
| 2090 SHEET T83 0.126-0.249 S | 70 | 11 | 11.4 | 100 | 126 | 88 | 104 | 63 | 71 | 37 | 75 | 65 | 73 | 70 | 66 | 4.3 | S | T83 | 0.094 | 4 | 5 | Sheet | 0.34 | AMS 4251 | 0.126-0.249 |
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