7050-T76511 Extrusion: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 7050 / T76511 / Extrusion |
| Specifications | AMS 4340 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.4.0, Table 3.7.4.0(e) (pdf page 331 of the chapter file) |
| Dimension bands | 6 |
| 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 | 0.000–0.499 in | 0.500–1.000 in | 1.001–2.000 in | 2.001–3.000 in | 3.001–4.000 in | 4.001–5.000 in | ||
|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4340 | AMS 4340 | AMS 4340 | AMS 4340 | AMS 4340 | AMS 4340 | ||
| Basis | A | B | S | S | S | S | S | |
| Ftu, ksi | L | 77 | 79 | 79 | 79 | 79 | 79 | 79 |
| LT | 76 | 78 | 77 | 75 | 73 | 71 | 68 | |
| Fty, ksi | L | 68 | 71 | 69 | 69 | 69 | 69 | 69 |
| LT | 67 | 69 | 67 | 65 | 63 | 61 | 59 | |
| Fcy, ksi | L | 68 | 71 | 69 | 69 | 69 | 69 | 69 |
| LT | 70 | 73 | 70 | 69 | 67 | 66 | 64 | |
| Fsu, ksi | L | 42 | 44 | 43 | 43 | 42 | 41 | 40 |
| LT | 42 | 44 | 43 | 43 | 42 | 41 | 40 | |
| Fbru (e/D = 1.5), ksi | L | 113 | 116 | 115 | 114 | 110 | 107 | 103 |
| LT | 113 | 116 | 115 | 114 | 110 | 107 | 103 | |
| Fbru (e/D = 2.0), ksi | L | 147 | 151 | 150 | 148 | 144 | 140 | 136 |
| LT | 147 | 151 | 150 | 148 | 144 | 140 | 136 | |
| Fbry (e/D = 1.5), ksi | L | 94 | 98 | 94 | 92 | 89 | 86 | 82 |
| LT | 94 | 98 | 94 | 92 | 89 | 86 | 82 | |
| Fbry (e/D = 2.0), ksi | L | 109 | 114 | 110 | 108 | 104 | 98 | 93 |
| LT | 109 | 114 | 110 | 108 | 104 | 98 | 93 | |
| e, % | L | 7 | 7 | 7 | 7 | 7 | 7 | 7 |
| LT | … | … | … | … | … | … | … | |
| E, Msi | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | 10.3 | |
| Ec, Msi | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | |
| G, Msi | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 7050 Tables
- 7050-T73511 Extrusion (Table 3.7.4.0(e))
- 7050-T74 Die forging (Table 3.7.4.0(c))
- 7050-T7451 Plate (Table 3.7.4.0(b))
- 7050-T74511 Extrusion (Table 3.7.4.0(e))
- 7050-T7452 Die forgings (Table 3.7.4.0(c))
- 7050-T7452 Hand Forging (Table 3.7.4.0(d))
- 7050-T7651 Plate (Table 3.7.4.0(b))
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.