2024-T42 Flat Sheet and Plate: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2024 / T42 / Flat Sheet and Plate |
| Specifications | AMS 4035 and AMS-QQ-A-250/4 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(b) (pdf page 72 of the chapter file) |
| Dimension bands | 5 |
| Density | 2768 kg/m³ |
Design Mechanical and Physical Properties (room temperature)
Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. 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 | 0.010–0.249 in (0.254–6.325 mm) | 0.250–0.499 in (6.35–12.67 mm) | 0.500–1.000 in (12.7–25.4 mm) | 1.001–2.000 in (25.43–50.8 mm) | 2.001–3.000 in (50.83–76.2 mm) | |
|---|---|---|---|---|---|---|
| Specification | AMS 4035 and AMS-QQ-A-250/4 | AMS 4035 and AMS-QQ-A-250/4 | AMS 4035 and AMS-QQ-A-250/4 | AMS 4035 and AMS-QQ-A-250/4 | AMS 4035 and AMS-QQ-A-250/4 | |
| Basis | S | S | S | S | S | |
| Ftu, MPa | L | 427.5 | 427.5 | 420.6 | 413.7 | … |
| LT | 427.5 | 427.5 | 420.6 | 413.7 | 399.9 | |
| Fty, MPa | L | 262 | 262 | 262 | 262 | … |
| LT | 262 | 262 | 262 | 262 | 262 | |
| Fcy, MPa | L | 289.6 | 289.6 | 275.8 | 255.1 | … |
| LT | 282.7 | 282.7 | 282.7 | 282.7 | … | |
| Fsu, MPa | L | 255.1 | 255.1 | 248.2 | 248.2 | … |
| LT | 255.1 | 255.1 | 248.2 | 248.2 | … | |
| Fbru (e/D = 1.5), MPa | L | 682.6 | 675.7 | 648.1 | 586.1 | … |
| LT | 682.6 | 675.7 | 648.1 | 586.1 | … | |
| Fbru (e/D = 2.0), MPa | L | 848.1 | 848.1 | 834.3 | 820.5 | … |
| LT | 848.1 | 848.1 | 834.3 | 820.5 | … | |
| Fbry (e/D = 1.5), MPa | L | 461.9 | 461.9 | 461.9 | 461.9 | … |
| LT | 461.9 | 461.9 | 461.9 | 461.9 | … | |
| Fbry (e/D = 2.0), MPa | L | 551.6 | 551.6 | 551.6 | 551.6 | … |
| LT | 551.6 | 551.6 | 551.6 | 551.6 | … | |
| e, % | L | … | … | … | … | … |
| LT | … | 12 | 8 | … | 4 | |
| E, GPa | 72.39 | 73.77 | 73.77 | 73.77 | … | |
| Ec, GPa | 73.77 | 75.15 | 75.15 | 75.15 | … | |
| G, GPa | 27.58 | 27.58 | 27.58 | 27.58 | … | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | … | |
| ρ, kg/m³ | 2768 | 2768 | 2768 | 2768 | … | |
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
| °C | F_tu | F_ty |
|---|---|---|
| 38 | 99.4 | 100 |
| 93 | 95.8 | 98 |
| 149 | 88.9 | 95 |
| 204 | 71.4 | 84 |
| 26 | 37.9 | 47.6 |
| 316 | 20.3 | 22.8 |
| 371 | 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 Extruded bar, rod, and shapes (Table 3.2.3.0(j))
- 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.