7010-T7451 Plate: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 7010 / T7451 / Plate |
| Specifications | AMS 4205 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.7.1.0, Table 3.7.1.0(b) (pdf page 295 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 | 0.250–1.000 in | 1.001–2.000 in | 2.001–3.000 in | 3.001–4.000 in | 4.001–5.000 in | 5.001–6.000 in | |||||
|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4205 | AMS 4205 | AMS 4205 | AMS 4205 | AMS 4205 | AMS 4205 | |||||
| Basis | S | S | A | B | A | B | A | B | A | B | |
| Ftu, ksi | L | 71 | 71 | 70 | 72 | 70 | 71 | 68 | 71 | 68 | 70 |
| LT | 72 | 72 | 71 | 72 | 70 | 72 | 69 | 71 | 67 | 71 | |
| ST | … | … | 66 | 68 | 66 | 68 | 65 | 67 | 63 | 67 | |
| Fty, ksi | L | 62 | 62 | 60 | 62 | 60 | 62 | 59 | 61 | 57 | 61 |
| LT | 62 | 62 | 60 | 62 | 59 | 61 | 58 | 60 | 57 | 60 | |
| ST | … | … | 55 | 57 | 54 | 56 | 53 | 55 | 52 | 54 | |
| Fcy, ksi | L | 61 | 61 | 59 | 61 | 58 | 60 | 57 | 59 | 56 | 59 |
| LT | 63 | 63 | 62 | 64 | 61 | 63 | 60 | 62 | 59 | 63 | |
| ST | … | … | 61 | 63 | 60 | 62 | 59 | 61 | 58 | 61 | |
| Fsu, ksi | L | 41 | 41 | 42 | 42 | 42 | 43 | 42 | 43 | 41 | 43 |
| LT | 41 | 41 | 42 | 42 | 42 | 43 | 42 | 43 | 41 | 43 | |
| ST | … | … | 42 | 42 | 42 | 43 | 42 | 43 | 41 | 43 | |
| Fbru (e/D = 1.5), ksi | L | 100 | 101 | 101 | 102 | 100 | 103 | 100 | 103 | 97 | 103 |
| LT | 100 | 101 | 101 | 102 | 100 | 103 | 100 | 103 | 97 | 103 | |
| ST | … | … | 101 | 102 | 100 | 103 | 100 | 103 | 97 | 103 | |
| Fbru (e/D = 2.0), ksi | L | 127 | 129 | 130 | 132 | 130 | 134 | 129 | 133 | 126 | 133 |
| LT | 127 | 129 | 130 | 132 | 130 | 134 | 129 | 133 | 126 | 133 | |
| ST | … | … | 130 | 132 | 130 | 134 | 129 | 133 | 126 | 133 | |
| Fbry (e/D = 1.5), ksi | L | 81 | 82 | 81 | 84 | 81 | 84 | 81 | 84 | 80 | 84 |
| LT | 81 | 82 | 81 | 84 | 81 | 84 | 81 | 84 | 80 | 84 | |
| ST | … | … | 81 | 84 | 81 | 84 | 81 | 84 | 80 | 84 | |
| Fbry (e/D = 2.0), ksi | L | 94 | 97 | 97 | 100 | 98 | 101 | 98 | 101 | 97 | 102 |
| LT | 94 | 97 | 97 | 100 | 98 | 101 | 98 | 101 | 97 | 102 | |
| ST | … | … | 97 | 100 | 98 | 101 | 98 | 101 | 97 | 102 | |
| e, % | L | 9 | 9 | 9 | 9 | 9 | 9 | 9 | 9 | 8 | 8 |
| LT | 6 | 6 | 6 | 6 | 6 | 6 | 5 | 5 | 5 | 5 | |
| ST | … | … | 2.5 | 2.5 | 2 | 2 | 2 | 2 | 2 | 2 | |
| E, Msi | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | |
| Ec, Msi | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | 10.6 | |
| 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 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | 0.102 | |
Effect of Temperature
Percent of the room-temperature value against temperature, digitized from the handbook figures (the shortest exposure of each figure, every 10 °F). Strength curves give the allowable at temperature; "after exposure" curves give the room-temperature property after a soak at that temperature.
Strength allowables at temperature, percent of room temperature
| °F | F_tu | F_ty |
|---|---|---|
| 100 | 97.2 | 99.5 |
| 200 | 85.3 | 92.8 |
| 300 | 72.5 | 80.2 |
Factors in percent of the room-temperature allowable.
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.