Tools › Materials › Aluminum › 2519-T87 Plate

2519-T87 Plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2519 / T87 / Plate
SpecificationsMIL-DTL-46192
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.11.0, Table 3.2.11.0(b) (pdf page 203 of the chapter file)
Dimension bands4
Density0.102 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 band0.250–1.000 in1.001–2.000 in2.001–3.000 in3.001–4.000 in
SpecificationMIL-DTL-46192MIL-DTL-46192MIL-DTL-46192MIL-DTL-46192
BasisSSSS
Ftu, ksiL66666768
LT68686868
ST63636362
Fty, ksiL59596061
LT58585959
ST55555555
Fcy, ksiL57575858
LT60606161
ST58585858
Fsu, ksiL42414140
LT42414140
ST42414140
Fbru (e/D = 1.5), ksiL105105104103
LT105105104103
ST105105104103
Fbru (e/D = 2.0), ksiL135134133131
LT135134133131
ST135134133131
Fbry (e/D = 1.5), ksiL85858787
LT85858787
ST85858787
Fbry (e/D = 2.0), ksiL9999100100
LT9999100100
ST9999100100
e, %L10987
LT7765
ST…………
E, Msi10.510.510.510.5
Ec, Msi10.810.810.810.8
G, Msi4444
ν0.330.330.330.33
ρ, lb/in30.1020.1020.1020.102

Effect of Temperature

The handbook maps no temperature-effect figure to this table.

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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.