2024-T81 Clad flat sheet and plate: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2024 / T81 / 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 78 of the chapter file) |
| Dimension bands | 2 |
| 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 | 0.010–0.062 in | 0.063–0.249 in | |
|---|---|---|---|
| Specification | AMS-QQ-A-250/5 | AMS-QQ-A-250/5 | |
| Basis | S | S | |
| Ftu, ksi | L | 64 | 67 |
| LT | 62 | 65 | |
| Fty, ksi | L | 57 | 59 |
| LT | 54 | 56 | |
| Fcy, ksi | L | 55 | 57 |
| LT | 55 | 57 | |
| Fsu, ksi | L | 38 | 39 |
| LT | 38 | 39 | |
| Fbru (e/D = 1.5), ksi | L | 96 | 100 |
| LT | 96 | 100 | |
| Fbru (e/D = 2.0), ksi | L | 122 | 127 |
| LT | 122 | 127 | |
| Fbry (e/D = 1.5), ksi | L | 78 | 83 |
| LT | 78 | 83 | |
| Fbry (e/D = 2.0), ksi | L | 90 | 94 |
| LT | 90 | 94 | |
| e, % | L | … | … |
| LT | 5 | 5 | |
| E, Msi | 10.5 | 10.5 | |
| Ec, Msi | 10.7 | 10.7 | |
| ν | 0.33 | 0.33 | |
| ρ, lb/in3 | 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 |
|---|---|---|---|---|---|---|
| 100 | 97.6 | 98.2 | 99.3 | 99.1 | 99.7 | 99.7 |
| 200 | 88.9 | 90.5 | 94.4 | 94 | 97.3 | 97.4 |
| 300 | 81.9 | 83.2 | 86.1 | 87.9 | 92.1 | 92.9 |
| 400 | 71.3 | 70.1 | 74.8 | 79.3 | ||
| 500 | 51.2 | 49.1 | ||||
| 600 | 28.5 | 24.8 | ||||
| 700 | 9.1 |
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 Clad flat sheet and plate (Table 3.2.3.0(e))
- 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 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.