5454-H112 Sheet and plate: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 5454 / H112 / Sheet and plate |
| Specifications | AMS-QQ-A-250/10 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.5.4.0, Table 3.5.4.0(b) (pdf page 248 of the chapter file) |
| Dimension bands | 2 |
| Density | 2685 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) | 0.500–3.000 in (12.7–76.2 mm) | |
|---|---|---|---|
| Specification | AMS-QQ-A-250/10 | AMS-QQ-A-250/10 | |
| Basis | S | S | |
| Ftu, MPa | L | 220.6 | 213.7 |
| LT | 220.6 | 213.7 | |
| Fty, MPa | L | 124.1 | 82.74 |
| LT | 124.1 | 82.74 | |
| Fcy, MPa | L | 117.2 | 82.74 |
| LT | 124.1 | 82.74 | |
| Fsu, MPa | L | 137.9 | 131 |
| LT | 137.9 | 131 | |
| Fbru (e/D = 1.5), MPa | L | 330.9 | 317.2 |
| LT | 330.9 | 317.2 | |
| Fbru (e/D = 2.0), MPa | L | 441.3 | 427.5 |
| LT | 441.3 | 427.5 | |
| Fbry (e/D = 1.5), MPa | L | 172.4 | 137.9 |
| LT | 172.4 | 137.9 | |
| Fbry (e/D = 2.0), MPa | L | 213.7 | 165.5 |
| LT | 213.7 | 165.5 | |
| e, % | L | 8 | 8 |
| LT | … | … | |
| E, GPa | 70.33 | 70.33 | |
| Ec, GPa | 71.71 | 71.71 | |
| G, GPa | 26.54 | 26.54 | |
| ν | 0.33 | 0.33 | |
| ρ, kg/m³ | 2685 | 2685 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 5454 Tables
- 5454-H111 Extrusion (Table 3.5.4.0(b))
- 5454-H112 Extrusion (Table 3.5.4.0(b))
- 5454-H32 Sheet and plate (Table 3.5.4.0(b))
- 5454-H34 Sheet and plate (Table 3.5.4.0(b))
- 5454-O Extrusion (Table 3.5.4.0(b))
- 5454-O Sheet and plate (Table 3.5.4.0(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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.