5086-H32 Sheet and 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 | 5086 / H32 / Sheet and plate |
| Specifications | AMS-QQ-A-250/7 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.5.3.0, Table 3.5.3.0(b) (pdf page 238 of the chapter file) |
| Dimension bands | 1 |
| Density | 2657 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 | 0.020–2.000 in (0.508–50.8 mm) | ||
|---|---|---|---|
| Specification | AMS-QQ-A-250/7 | ||
| Basis | A | B | |
| Ftu, MPa | L | 275.8 | 282.7 |
| LT | 275.8 | 282.7 | |
| Fty, MPa | L | 193.1 | 206.8 |
| LT | 179.3 | 193.1 | |
| Fcy, MPa | L | 179.3 | 193.1 |
| LT | 193.1 | 206.8 | |
| Fsu, MPa | L | 165.5 | 172.4 |
| LT | 165.5 | 172.4 | |
| Fbru (e/D = 1.5), MPa | L | 399.9 | 420.6 |
| LT | 399.9 | 420.6 | |
| Fbru (e/D = 2.0), MPa | L | 551.6 | 565.4 |
| LT | 551.6 | 565.4 | |
| Fbry (e/D = 1.5), MPa | L | 268.9 | 289.6 |
| LT | 268.9 | 289.6 | |
| Fbry (e/D = 2.0), MPa | L | 330.9 | 351.6 |
| LT | 330.9 | 351.6 | |
| E, GPa | 70.33 | 70.33 | |
| Ec, GPa | 71.71 | 71.71 | |
| G, GPa | 26.54 | 26.54 | |
| ρ, kg/m³ | 2657 | 2657 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 5086 Tables
- 5086-H111 Extrusion (Table 3.5.3.0(b))
- 5086-H112 Extrusion (Table 3.5.3.0(b))
- 5086-H112 Sheet and plate (Table 3.5.3.0(b))
- 5086-H34 Sheet and plate (Table 3.5.3.0(b))
- 5086-H36 Sheet and plate (Table 3.5.3.0(b))
- 5086-H38 Sheet and plate (Table 3.5.3.0(b))
- 5086-O Extrusion (Table 3.5.3.0(b))
- 5086-O Sheet and plate (Table 3.5.3.0(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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.