Aerospace Materials: MG-AZ31B SHEET H24
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) | Fsu ksi (ksi) | 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 (%) | form | poisson ratio | specification | thickness range |
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| MG-AZ31B SHEET H24 0.016-0.062 S | 70 | 6.5 | 6.5 | 58 | 68 | 43 | 43 | — | 18 | 39 | 40 | 29 | 32 | 2.4 | S | H24 | 0.0639 | 6 | Sheet | 0.35 | AMS 4377 | 0.016-0.062 |
| MG-AZ31B SHEET H24 0.063-0.249 S | 70 | 6.5 | 6.5 | 58 | 68 | 43 | 43 | 24 | 18 | 39 | 40 | 29 | 32 | 2.4 | S | H24 | 0.0639 | 6 | Sheet | 0.35 | AMS 4377 | 0.063-0.249 |
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