2024-T42 Extruded bar, rod, and shapes: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2024 / T42 / Extruded bar, rod, and shapes |
| Specifications | AMS-QQ-A-200/3 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(j) (pdf page 86 of the chapter file) |
| Dimension bands | 10 |
| 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 | 0.000–0.249 in, area 0–25 in2 | 0.250–0.499 in, area 0–25 in2 | 0.500–0.749 in, area 0–25 in2 | 0.750–0.999 in, area 0–25 in2 | 1.000–1.249 in, area 0–25 in2 | 1.250–1.499 in, area 0–25 in2 | 1.500–1.749 in, area 0–25 in2 | 1.750–1.999 in, area 0–25 in2 | 2.000–2.249 in, area 0–25 in2 | 2.250–2.499 in, area 0–25 in2 | |
|---|---|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | AMS-QQ-A-200/3 | |
| Basis | S | S | S | S | S | S | S | S | S | S | |
| Ftu, ksi | L | 57 | 57 | 57 | 57 | 57 | 57 | 57 | 57 | 57 | 57 |
| LT | 55 | 54 | 52 | 51 | 49 | 47 | 45 | 43 | 41 | 39 | |
| Fty, ksi | L | 38 | 38 | 38 | 38 | 38 | 38 | 38 | 38 | 38 | 38 |
| LT | 36 | 35 | 34 | 33 | 32 | 31 | 30 | 29 | 28 | 27 | |
| Fcy, ksi | L | 38 | 38 | 38 | 38 | 38 | 38 | 38 | 38 | 38 | 38 |
| LT | 39 | 38 | 37 | 36 | 35 | 34 | 33 | 31 | 30 | 29 | |
| Fsu, ksi | L | 29 | 29 | 29 | 29 | 29 | 29 | 28 | 27 | 26 | 24 |
| LT | 29 | 29 | 29 | 29 | 29 | 29 | 28 | 27 | 26 | 24 | |
| Fbru (e/D = 1.5), ksi | L | 81 | 80 | 79 | 77 | 75 | 74 | 71 | 69 | 67 | 64 |
| LT | 81 | 80 | 79 | 77 | 75 | 74 | 71 | 69 | 67 | 64 | |
| Fbru (e/D = 2.0), ksi | L | 99 | 98 | 97 | 95 | 93 | 91 | 89 | 86 | 83 | 81 |
| LT | 99 | 98 | 97 | 95 | 93 | 91 | 89 | 86 | 83 | 81 | |
| Fbry (e/D = 1.5), ksi | L | 56 | 55 | 53 | 51 | 49 | 47 | 44 | 41 | 39 | 36 |
| LT | 56 | 55 | 53 | 51 | 49 | 47 | 44 | 41 | 39 | 36 | |
| Fbry (e/D = 2.0), ksi | L | 69 | 67 | 65 | 63 | 61 | 59 | 56 | 53 | 50 | 47 |
| LT | 69 | 67 | 65 | 63 | 61 | 59 | 56 | 53 | 50 | 47 | |
| e, % | L | 12 | 12 | 12 | 10 | 10 | 10 | 10 | 10 | 10 | 10 |
| LT | … | … | … | … | … | … | … | … | … | … | |
| E, Msi | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | 10.8 | |
| Ec, Msi | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | 11 | |
| G, Msi | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | 4.1 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.1 | 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 |
|---|---|---|
| 100 | 99.4 | 100 |
| 200 | 95.8 | 98 |
| 300 | 88.9 | 95 |
| 400 | 71.4 | 84 |
| 500 | 37.9 | 47.6 |
| 600 | 20.3 | 22.8 |
| 700 | 11.8 | 12.9 |
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 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.