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 | 0.102 lb/in3 |
Design Mechanical and Physical Properties (room temperature)
As printed in the handbook table. 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 | 1.001–2.000 in | 2.001–3.000 in | 3.001–4.000 in | |
|---|---|---|---|---|---|
| Specification | MIL-DTL-46192 | MIL-DTL-46192 | MIL-DTL-46192 | MIL-DTL-46192 | |
| Basis | S | S | S | S | |
| Ftu, ksi | L | 66 | 66 | 67 | 68 |
| LT | 68 | 68 | 68 | 68 | |
| ST | 63 | 63 | 63 | 62 | |
| Fty, ksi | L | 59 | 59 | 60 | 61 |
| LT | 58 | 58 | 59 | 59 | |
| ST | 55 | 55 | 55 | 55 | |
| Fcy, ksi | L | 57 | 57 | 58 | 58 |
| LT | 60 | 60 | 61 | 61 | |
| ST | 58 | 58 | 58 | 58 | |
| Fsu, ksi | L | 42 | 41 | 41 | 40 |
| LT | 42 | 41 | 41 | 40 | |
| ST | 42 | 41 | 41 | 40 | |
| Fbru (e/D = 1.5), ksi | L | 105 | 105 | 104 | 103 |
| LT | 105 | 105 | 104 | 103 | |
| ST | 105 | 105 | 104 | 103 | |
| Fbru (e/D = 2.0), ksi | L | 135 | 134 | 133 | 131 |
| LT | 135 | 134 | 133 | 131 | |
| ST | 135 | 134 | 133 | 131 | |
| Fbry (e/D = 1.5), ksi | L | 85 | 85 | 87 | 87 |
| LT | 85 | 85 | 87 | 87 | |
| ST | 85 | 85 | 87 | 87 | |
| Fbry (e/D = 2.0), ksi | L | 99 | 99 | 100 | 100 |
| LT | 99 | 99 | 100 | 100 | |
| ST | 99 | 99 | 100 | 100 | |
| e, % | L | 10 | 9 | 8 | 7 |
| LT | 7 | 7 | 6 | 5 | |
| ST | … | … | … | … | |
| E, Msi | 10.5 | 10.5 | 10.5 | 10.5 | |
| Ec, Msi | 10.8 | 10.8 | 10.8 | 10.8 | |
| G, Msi | 4 | 4 | 4 | 4 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.102 | 0.102 | 0.102 | 0.102 | |
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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.