2519-T87 Plate: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2519 / T87 / Plate |
| Specifications | MIL-DTL-46192 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.11.0, Table 3.2.11.0(b) (pdf page 203 of the chapter file) |
| Dimension bands | 4 |
| Density | 2823 kg/m³ |
Design Mechanical and Physical Properties (room temperature)
Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. Bases: A and B are statistical minimums (99 % and 90 % probability at 95 % confidence), S the specification minimum. Grain directions: L longitudinal, LT long transverse, ST short transverse.
| Dimension band | 0.250–1.000 in (6.35–25.4 mm) | 1.001–2.000 in (25.43–50.8 mm) | 2.001–3.000 in (50.83–76.2 mm) | 3.001–4.000 in (76.23–101.6 mm) | |
|---|---|---|---|---|---|
| Specification | MIL-DTL-46192 | MIL-DTL-46192 | MIL-DTL-46192 | MIL-DTL-46192 | |
| Basis | S | S | S | S | |
| Ftu, MPa | L | 455.1 | 455.1 | 461.9 | 468.8 |
| LT | 468.8 | 468.8 | 468.8 | 468.8 | |
| ST | 434.4 | 434.4 | 434.4 | 427.5 | |
| Fty, MPa | L | 406.8 | 406.8 | 413.7 | 420.6 |
| LT | 399.9 | 399.9 | 406.8 | 406.8 | |
| ST | 379.2 | 379.2 | 379.2 | 379.2 | |
| Fcy, MPa | L | 393 | 393 | 399.9 | 399.9 |
| LT | 413.7 | 413.7 | 420.6 | 420.6 | |
| ST | 399.9 | 399.9 | 399.9 | 399.9 | |
| Fsu, MPa | L | 289.6 | 282.7 | 282.7 | 275.8 |
| LT | 289.6 | 282.7 | 282.7 | 275.8 | |
| ST | 289.6 | 282.7 | 282.7 | 275.8 | |
| Fbru (e/D = 1.5), MPa | L | 723.9 | 723.9 | 717.1 | 710.2 |
| LT | 723.9 | 723.9 | 717.1 | 710.2 | |
| ST | 723.9 | 723.9 | 717.1 | 710.2 | |
| Fbru (e/D = 2.0), MPa | L | 930.8 | 923.9 | 917 | 903.2 |
| LT | 930.8 | 923.9 | 917 | 903.2 | |
| ST | 930.8 | 923.9 | 917 | 903.2 | |
| Fbry (e/D = 1.5), MPa | L | 586.1 | 586.1 | 599.8 | 599.8 |
| LT | 586.1 | 586.1 | 599.8 | 599.8 | |
| ST | 586.1 | 586.1 | 599.8 | 599.8 | |
| Fbry (e/D = 2.0), MPa | L | 682.6 | 682.6 | 689.5 | 689.5 |
| LT | 682.6 | 682.6 | 689.5 | 689.5 | |
| ST | 682.6 | 682.6 | 689.5 | 689.5 | |
| e, % | L | 10 | 9 | 8 | 7 |
| LT | 7 | 7 | 6 | 5 | |
| ST | … | … | … | … | |
| E, GPa | 72.39 | 72.39 | 72.39 | 72.39 | |
| Ec, GPa | 74.46 | 74.46 | 74.46 | 74.46 | |
| G, GPa | 27.58 | 27.58 | 27.58 | 27.58 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, kg/m³ | 2823 | 2823 | 2823 | 2823 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Source and Use
U.S. Department of Defense (2003). Metallic Materials and Elements for Aerospace Vehicle Structures. MIL-HDBK-5J, 31 January 2003 (public domain). The values are the handbook's design allowables as extracted from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ. No warranty is given.