2014-T62 Sheet: MIL-HDBK-5J Design Allowables
show SI units (MPa, GPa, kg/m³) open the MIL-HDBK-5J tool compare against temperature find alternatives
| Material class | Aluminum |
| Alloy / temper / form | 2014 / T62 / Sheet |
| 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 | 0.101 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 | 0.020–0.039 in | 0.040–0.249 in | |||
|---|---|---|---|---|---|
| Specification | AMS 4028 | AMS 4028 | |||
| Basis | A | B | A | B | |
| Ftu, ksi | L | 65 | 67 | 67 | 68 |
| LT | 64 | 66 | 66 | 67 | |
| Fty, ksi | L | 58 | 60 | 59 | 60 |
| LT | 57 | 59 | 58 | 59 | |
| Fcy, ksi | L | 58 | 60 | 59 | 60 |
| LT | 59 | 61 | 60 | 61 | |
| Fsu, ksi | L | 39 | 40 | 40 | 41 |
| LT | 39 | 40 | 40 | 41 | |
| Fbru (e/D = 1.5), ksi | L | 97 | 100 | 100 | 102 |
| LT | 97 | 100 | 100 | 102 | |
| Fbru (e/D = 2.0), ksi | L | 123 | 127 | 127 | 129 |
| LT | 123 | 127 | 127 | 129 | |
| Fbry (e/D = 1.5), ksi | L | 81 | 84 | 83 | 84 |
| LT | 81 | 84 | 83 | 84 | |
| Fbry (e/D = 2.0), ksi | L | 93 | 96 | 95 | 96 |
| LT | 93 | 96 | 95 | 96 | |
| e, % | L | … | … | … | … |
| LT | 6 | 6 | 7 | 7 | |
| E, Msi | 10.5 | 10.5 | 10.5 | 10.5 | |
| Ec, Msi | 10.7 | 10.7 | 10.7 | 10.7 | |
| G, Msi | 4 | 4 | 4 | 4 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.101 | 0.101 | 0.101 | 0.101 | |
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 Plate (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.