7049/7149-T73 Die forging: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 7049/7149 / T73 / Die forging |
| Specifications | AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.3.0, Table 3.7.3.0(c) (pdf page 307 of the chapter file) |
| Dimension bands | 5 |
| Density | 0.103 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 | 0–1 in | 1.001–2.000 in | 2.001–3.000 in | 3.001–4.000 in | 4.001–5.000 in | ||||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771 | AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771 | AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771 | AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771 | AMS-QQ-A-367, AMS 4111, AMS 4320, and AMS-A-22771 | ||||||
| Basis | A | B | A | B | A | B | A | B | A | B | |
| Ftu, ksi | L | 71 | 74 | 70 | 73 | 69 | 72 | 68 | 71 | 67 | 70 |
| LT | 71 | … | 70 | … | 70 | … | 70 | … | 68 | … | |
| ST | … | … | … | … | … | … | … | … | … | … | |
| Fty, ksi | L | 60 | 64 | 59 | 63 | 58 | 61 | 57 | 60 | 55 | 59 |
| LT | 61 | … | 60 | … | 60 | … | 60 | … | 58 | … | |
| ST | … | … | … | … | … | … | … | … | … | … | |
| Fcy, ksi | L | 62 | 66 | 61 | 65 | 60 | 63 | 59 | 62 | 57 | 61 |
| LT | … | … | … | … | … | … | … | … | … | … | |
| ST | 56 | 60 | 55 | 59 | 54 | 57 | 53 | 56 | 51 | 55 | |
| Fsu, ksi | L | 40 | 41 | 39 | 41 | 39 | 40 | 38 | 40 | 37 | 39 |
| LT | 40 | … | 39 | … | 39 | … | 38 | … | 37 | … | |
| ST | 40 | 41 | 39 | 41 | 39 | 40 | 38 | 40 | 37 | 39 | |
| Fbru (e/D = 1.5), ksi | L | 100 | 105 | 99 | 103 | 98 | 102 | 96 | 100 | 95 | 99 |
| LT | 100 | … | 99 | … | 98 | … | 96 | … | 95 | … | |
| ST | 100 | 105 | 99 | 103 | 98 | 102 | 96 | 100 | 95 | 99 | |
| Fbru (e/D = 2.0), ksi | L | 132 | 138 | 130 | 136 | 128 | 134 | 126 | 132 | 125 | 130 |
| LT | 132 | … | 130 | … | 128 | … | 126 | … | 125 | … | |
| ST | 132 | 138 | 130 | 136 | 128 | 134 | 126 | 132 | 125 | 130 | |
| Fbry (e/D = 1.5), ksi | L | 82 | 82 | 75 | 80 | 74 | 78 | 73 | 76 | 70 | 75 |
| LT | 82 | … | 75 | … | 74 | … | 73 | … | 70 | … | |
| ST | 82 | 82 | 75 | 80 | 74 | 78 | 73 | 76 | 70 | 75 | |
| Fbry (e/D = 2.0), ksi | L | 99 | 99 | 91 | 97 | 90 | 94 | 88 | 93 | 85 | 91 |
| LT | 99 | … | 91 | … | 90 | … | 88 | … | 85 | … | |
| ST | 99 | 99 | 91 | 97 | 90 | 94 | 88 | 93 | 85 | 91 | |
| e, % | L | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 7 | 7 |
| LT | 3 | … | 3 | … | 3 | … | 2 | … | 2 | … | |
| ST | … | … | … | … | … | … | … | … | … | … | |
| E, Msi | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | |
| Ec, Msi | 10.7 | 10.7 | 10.7 | 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 | 3.9 | 3.9 | 3.9 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 7049/7149 Tables
- 7049/7149-T73 Hand forging (Table 3.7.3.0(d))
- 7049/7149-T73511 Extrusion (Table 3.7.3.0(e))
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.