2024-T351 Clad flat sheet and plate: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2024 / T351 / Clad flat sheet and plate |
| Specifications | AMS-QQ-A-250/5 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(e) (pdf page 75 of the chapter file) |
| Dimension bands | 6 |
| Density | 0.1 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 | 0.250–0.499 in | 0.500–1.000 in | 1.001–1.500 in | 1.501–2.000 in | 2.001–3.000 in | 3.001–4.000 in | |||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS-QQ-A-250/5 | AMS-QQ-A-250/5 | AMS-QQ-A-250/5 | AMS-QQ-A-250/5 | AMS-QQ-A-250/5 | AMS-QQ-A-250/5 | |||||||
| Basis | A | B | A | B | A | B | A | B | A | B | A | B | |
| Ftu, ksi | L | 62 | 64 | 61 | 63 | 60 | 62 | 60 | 62 | 58 | 60 | 55 | 57 |
| LT | 62 | 64 | 61 | 63 | 60 | 62 | 60 | 62 | 58 | 60 | 55 | 57 | |
| ST | … | … | … | … | … | … | … | … | 52 | 54 | 49 | 51 | |
| Fty, ksi | L | 46 | 48 | 45 | 48 | 45 | 48 | 45 | 47 | 44 | 46 | 39 | 41 |
| LT | 40 | 42 | 40 | 42 | 40 | 42 | 40 | 42 | 40 | 42 | 39 | 41 | |
| ST | … | … | … | … | … | … | … | … | 38 | 40 | 38 | 39 | |
| Fcy, ksi | L | 37 | 39 | 37 | 39 | 37 | 39 | 36 | 38 | 35 | 37 | 33 | 35 |
| LT | 43 | 45 | 42 | 45 | 42 | 44 | 42 | 44 | 41 | 43 | 39 | 41 | |
| ST | … | … | … | … | … | … | … | … | 46 | 48 | 44 | 47 | |
| Fsu, ksi | L | 37 | 38 | 36 | 37 | 35 | 37 | 35 | 37 | 34 | 35 | 32 | 34 |
| LT | 37 | 38 | 36 | 37 | 35 | 37 | 35 | 37 | 34 | 35 | 32 | 34 | |
| ST | … | … | … | … | … | … | … | … | 34 | 35 | 32 | 34 | |
| Fbru (e/D = 1.5), ksi | L | 94 | 97 | 92 | 95 | 91 | 94 | 91 | 94 | 88 | 91 | 83 | 86 |
| LT | 94 | 97 | 92 | 95 | 91 | 94 | 91 | 94 | 88 | 91 | 83 | 86 | |
| ST | … | … | … | … | … | … | … | … | 88 | 91 | 83 | 86 | |
| Fbru (e/D = 2.0), ksi | L | 115 | 119 | 113 | 117 | 111 | 115 | 111 | 115 | 107 | 111 | 102 | 106 |
| LT | 115 | 119 | 113 | 117 | 111 | 115 | 111 | 115 | 107 | 111 | 102 | 106 | |
| ST | … | … | … | … | … | … | … | … | 107 | 111 | 102 | 106 | |
| Fbry (e/D = 1.5), ksi | L | 69 | 72 | 69 | 72 | 69 | 72 | 69 | 72 | 69 | 72 | 67 | 70 |
| LT | 69 | 72 | 69 | 72 | 69 | 72 | 69 | 72 | 69 | 72 | 67 | 70 | |
| ST | … | … | … | … | … | … | … | … | 69 | 72 | 67 | 70 | |
| Fbry (e/D = 2.0), ksi | L | 82 | 86 | 82 | 86 | 82 | 86 | 82 | 86 | 82 | 86 | 80 | 84 |
| LT | 82 | 86 | 82 | 86 | 82 | 86 | 82 | 86 | 82 | 86 | 80 | 84 | |
| ST | … | … | … | … | … | … | … | … | 82 | 86 | 80 | 84 | |
| e, % | L | … | … | … | … | … | … | … | … | … | … | … | … |
| LT | 12 | 12 | 8 | 8 | 7 | 7 | 6 | 6 | 4 | 4 | 4 | 4 | |
| ST | … | … | … | … | … | … | … | … | … | … | … | … | |
| E, Msi | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | 10.7 | |
| Ec, Msi | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | 10.9 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | 0.1 | |
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
Moduli at temperature
Elongation and exposure effects
| °F | F_tu | F_ty | F_cy | F_su | F_bru | F_bry |
|---|---|---|---|---|---|---|
| -300 | 111.6 | 118.5 | ||||
| -200 | 105.3 | 108.3 | ||||
| -100 | 103 | 103.6 | ||||
| 0 | 101.6 | 102 | ||||
| 100 | 98.9 | 98.9 | 99.3 | 98.9 | 99.3 | 99.6 |
| 200 | 92.4 | 93.9 | 96.6 | 94.8 | 96.5 | 98 |
| 300 | 83.9 | 87.4 | 92.4 | 89.6 | 91 | 95.2 |
| 400 | 74.5 | 77.7 | 85.7 | 81.9 | 79.4 | 88.8 |
| 500 | 43.8 | 51.6 | 67.1 | 54.4 | 53.9 | 63.7 |
| 600 | 22.5 | 26.9 | 37.9 | 25.8 | 29.9 | 34.9 |
| 700 | 12 | 14 | 15.8 | 16.7 | ||
| 800 | 8 |
Factors in percent of the room-temperature allowable.
Other 2024 Tables
- 2024-T3 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T3 Drawn tubing (Table 3.2.3.0(g))
- 2024-T3 Sheet (Table 3.2.3.0(b))
- 2024-T3, T3510, and T3511 Extruded bar, rod, and shapes (Table 3.2.3.0(j))
- 2024-T351 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T351 Plate (Table 3.2.3.0(b))
- 2024-T361 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T361 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T361 Plate (Table 3.2.3.0(b))
- 2024-T361 Sheet (Table 3.2.3.0(b))
- 2024-T4 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T4 Clad coiled sheet (Table 3.2.3.0(e))
- 2024-T4 Coiled Sheet (Table 3.2.3.0(b))
- 2024-T42 Bar and rod; rolled, drawn, or cold-finished (Table 3.2.3.0(i))
- 2024-T42 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T42 Drawn tubing (Table 3.2.3.0(g))
- 2024-T42 Extruded bar, rod, and shapes (Table 3.2.3.0(j))
- 2024-T42 Flat Sheet and Plate (Table 3.2.3.0(b))
- 2024-T6 Bar and rod; rolled, drawn, or cold finished (Table 3.2.3.0(i))
- 2024-T62 Bar and rod; rolled, drawn, or cold finished (Table 3.2.3.0(i))
- 2024-T62 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T62 Flat Sheet and Plate (Table 3.2.3.0(b))
- 2024-T72 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T72 Flat Sheet and Plate (Table 3.2.3.0(b))
- 2024-T81 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T81 Drawn tubing (Table 3.2.3.0(g))
- 2024-T81 Sheet (Table 3.2.3.0(b))
- 2024-T81, T8510, and T8511 Extruded bar, rod, and shapes (Table 3.2.3.0(j))
- 2024-T851 Bar and rod; rolled, drawn, or cold finished (Table 3.2.3.0(i))
- 2024-T851 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T851 Plate (Table 3.2.3.0(b))
- 2024-T861 Clad flat sheet and plate (Table 3.2.3.0(e))
- 2024-T861 Plate (Table 3.2.3.0(b))
- 2024-T861 Sheet (Table 3.2.3.0(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.