Aerospace Materials: CLAD 2024 SHEET T351
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) | Fcy ksi ST (ksi) | Fsu ksi (ksi) | Ftu ksi (ksi) | Ftu ksi LT (ksi) | Ftu ksi ST (ksi) | Fty ksi (ksi) | Fty ksi LT (ksi) | Fty ksi ST (ksi) | basis | condition | density lb in3 (lb/in^3) | elongation pct LT (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| CLAD 2024 SHEET T351 3.001-4.000 A | 70 | 10.2 | 10.4 | 83 | 102 | 67 | 80 | 33 | 39 | 44 | 32 | 55 | 55 | 49 | 39 | 39 | 38 | A | T351 | 0.1 | 4 | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 3.001-4.000a |
| CLAD 2024 SHEET T351 3.001-4.000 B | 70 | 10.2 | 10.4 | 86 | 106 | 70 | 84 | 35 | 41 | 47 | 34 | 57 | 57 | 51 | 41 | 41 | 39 | B | T351 | 0.1 | — | Flat sheet and plate | 0.33 | AMS-QQ-A-250/5 | 3.001-4.000a |
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