2014-T62 Plate: MIL-HDBK-5J Design Allowables
show US units (ksi, Msi, lb/in³) open the MIL-HDBK-5J tool compare against temperature find alternatives
| Material class | Aluminum |
| Alloy / temper / form | 2014 / T62 / Plate |
| Specifications | AMS 4028 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.1.0, Table 3.2.1.0(b) (pdf page 29 of the chapter file) |
| Dimension bands | 2 |
| Density | 2796 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 | 0.250–0.499 in (6.35–12.67 mm) | 0.500–1.000 in (12.7–25.4 mm) | |||
|---|---|---|---|---|---|
| Specification | AMS 4028 | AMS 4028 | |||
| Basis | A | B | A | B | |
| Ftu, MPa | L | 448.2 | 461.9 | 448.2 | 461.9 |
| LT | 461.9 | 475.7 | 461.9 | 475.7 | |
| Fty, MPa | L | 393 | 406.8 | 393 | 406.8 |
| LT | 406.8 | 420.6 | 406.8 | 420.6 | |
| Fcy, MPa | L | 406.8 | 420.6 | 406.8 | 420.6 |
| LT | 413.7 | 427.5 | 413.7 | 427.5 | |
| Fsu, MPa | L | 255.1 | 268.9 | 255.1 | 268.9 |
| LT | 255.1 | 268.9 | 255.1 | 268.9 | |
| Fbru (e/D = 1.5), MPa | L | 689.5 | 710.2 | 689.5 | 710.2 |
| LT | 689.5 | 710.2 | 689.5 | 710.2 | |
| Fbru (e/D = 2.0), MPa | L | 875.6 | 903.2 | 875.6 | 903.2 |
| LT | 875.6 | 903.2 | 875.6 | 903.2 | |
| Fbry (e/D = 1.5), MPa | L | 579.2 | 599.8 | 579.2 | 599.8 |
| LT | 579.2 | 599.8 | 579.2 | 599.8 | |
| Fbry (e/D = 2.0), MPa | L | 682.6 | 710.2 | 682.6 | 710.2 |
| LT | 682.6 | 710.2 | 682.6 | 710.2 | |
| e, % | L | … | … | … | … |
| LT | 7 | 7 | 6 | 6 | |
| E, GPa | 73.77 | 73.77 | 73.77 | 73.77 | |
| Ec, GPa | 75.15 | 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 | 2796 | 2796 | 2796 | 2796 | |
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.
Moduli at temperature
Other 2014 Tables
- 2014-T6 Clad sheet (Table 3.2.1.0(c))
- 2014-T6 Die forging (Table 3.2.1.0(e))
- 2014-T6 Hand forging (Table 3.2.1.0(f))
- 2014-T6 Sheet (Table 3.2.1.0(b))
- 2014-T6 and T651 Bar, rod, and shapes, rolled, drawn, or cold-finished (Table 3.2.1.0(d))
- 2014-T6, T6510, and T6511 Extruded bar, rod, and shapes (Table 3.2.1.0(g))
- 2014-T62 Bar, rod, and shapes, rolled, drawn, or cold-finished (Table 3.2.1.0(d))
- 2014-T62 Clad plate (Table 3.2.1.0(c))
- 2014-T62 Clad sheet (Table 3.2.1.0(c))
- 2014-T62 Extruded bar, rod, and shapes (Table 3.2.1.0(g))
- 2014-T62 Sheet (Table 3.2.1.0(b))
- 2014-T651 Clad plate (Table 3.2.1.0(c))
- 2014-T651 Plate (Table 3.2.1.0(b))
- 2014-T652 Die forging (Table 3.2.1.0(e))
- 2014-T652 Hand forging (Table 3.2.1.0(f))
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.