2219-T852 Hand Forging: MIL-HDBK-5J Design Allowables
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| Material class | Aluminum |
| Alloy / temper / form | 2219 / T852 / Hand Forging |
| Specifications | AMS 4144 |
| Handbook | MIL-HDBK-5J, 31 January 2003, section 3.2.8.0, Table 3.2.8.0(c) (pdf page 171 of the chapter file) |
| Dimension bands | 8 |
| Density | 0.103 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 | 0–2 in | 2–4 in | 4.001–6.000 in | 6.001–8.000 in | 8.001–10.000 in | 10.001–12.000 in | 12.001–14.000 in | 14.001–17.000 in | |
|---|---|---|---|---|---|---|---|---|---|
| Specification | AMS 4144 | AMS 4144 | AMS 4144 | AMS 4144 | AMS 4144 | AMS 4144 | AMS 4144 | AMS 4144 | |
| Basis | S | S | S | S | S | S | S | S | |
| Ftu, ksi | L | 62 | 62 | 58 | 57 | 56 | 54 | 53 | 51 |
| LT | 62 | 62 | 56 | 55 | 54 | 53 | 52 | 50 | |
| ST | … | 60 | 56 | 55 | 54 | 53 | 52 | 50 | |
| Fty, ksi | L | 50 | 50 | 44 | 43 | 42 | 41 | 40 | 39 |
| LT | 49 | 49 | 42 | 41 | 41 | 40 | 40 | 39 | |
| ST | … | 46 | 41 | 40 | 39 | 39 | 38 | 37 | |
| Fcy, ksi | L | … | 46 | 40 | 39 | … | … | … | … |
| LT | … | 47 | 40 | 39 | … | … | … | … | |
| ST | … | 47 | 41 | 40 | … | … | … | … | |
| Fsu, ksi | L | … | 37 | 35 | 35 | … | … | … | … |
| LT | … | 37 | 35 | 35 | … | … | … | … | |
| ST | … | 37 | 35 | 35 | … | … | … | … | |
| Fbru (e/D = 1.5), ksi | L | … | … | … | 80 | … | … | … | … |
| LT | … | … | … | 80 | … | … | … | … | |
| ST | … | … | … | 80 | … | … | … | … | |
| Fbru (e/D = 2.0), ksi | L | … | 104 | 100 | 102 | … | … | … | … |
| LT | … | 104 | 100 | 102 | … | … | … | … | |
| ST | … | 104 | 100 | 102 | … | … | … | … | |
| Fbry (e/D = 1.5), ksi | L | … | 76 | 65 | 64 | … | … | … | … |
| LT | … | 76 | 65 | 64 | … | … | … | … | |
| ST | … | 76 | 65 | 64 | … | … | … | … | |
| Fbry (e/D = 2.0), ksi | L | … | 89 | 76 | 75 | … | … | … | … |
| LT | … | 89 | 76 | 75 | … | … | … | … | |
| ST | … | 89 | 76 | 75 | … | … | … | … | |
| e, % | L | … | … | … | … | … | … | … | … |
| LT | 4 | 4 | 4 | 4 | 3 | 3 | 3 | 3 | |
| ST | … | 3 | 3 | 3 | 3 | 2 | 2 | 2 | |
| E, Msi | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | 10.2 | |
| Ec, Msi | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | 10.4 | |
| G, Msi | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | 3.9 | |
| ν | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | 0.33 | |
| ρ, lb/in3 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | 0.103 | |
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-T8511 Extruded shapes (Table 3.2.8.0(d))
- 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.