2219-T8511 Extruded shapes: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2219 / T8511 / Extruded shapes |
| Specifications | AMS 4162 and AMS 4163 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.8.0, Table 3.2.8.0(d) (pdf page 172 of the chapter file) |
| Dimension bands | 2 |
| Density | 2851 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 | 0.000–0.499 in (0–12.67 mm), area 0–25 in2 (0–16130 mm²) | 0.500–2.999 in (12.7–76.17 mm), area 0–25 in2 (0–16130 mm²) | |
|---|---|---|---|
| Specification | AMS 4162 and AMS 4163 | AMS 4162 and AMS 4163 | |
| Basis | S | S | |
| Ftu, MPa | L | 399.9 | 399.9 |
| LT | 386.1 | 386.1 | |
| Fty, MPa | L | 289.6 | 289.6 |
| LT | 268.9 | 268.9 | |
| Fcy, MPa | L | 296.5 | 289.6 |
| LT | 296.5 | 282.7 | |
| Fsu, MPa | L | 227.5 | 227.5 |
| LT | 227.5 | 227.5 | |
| Fbru (e/D = 1.5), MPa | L | 599.8 | 558.5 |
| LT | 599.8 | 558.5 | |
| Fbru (e/D = 2.0), MPa | L | 779.1 | 737.7 |
| LT | 779.1 | 737.7 | |
| Fbry (e/D = 1.5), MPa | L | 475.7 | 461.9 |
| LT | 475.7 | 461.9 | |
| Fbry (e/D = 2.0), MPa | L | 579.2 | 565.4 |
| LT | 579.2 | 565.4 | |
| e, % | L | 6 | 6 |
| LT | 4 | 4 | |
| E, GPa | 72.39 | 72.39 | |
| Ec, GPa | 74.46 | 74.46 | |
| G, GPa | 27.58 | 27.58 | |
| ν | 0.33 | 0.33 | |
| ρ, kg/m³ | 2851 | 2851 | |
Effect of Temperature
The handbook maps no temperature-effect figure to this table.
Other 2219 Tables
- 2219-T62 Sheet and plate (Table 3.2.8.0(b))
- 2219-T81 Sheet and plate (Table 3.2.8.0(b))
- 2219-T851 Sheet and plate (Table 3.2.8.0(b))
- 2219-T852 Hand Forging (Table 3.2.8.0(c))
- 2219-T87 Plate (Table 3.2.8.0(b))
- 2219-T87 Sheet (Table 3.2.8.0(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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.