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7055-T76511 Extrusion: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7055 / T76511 / Extrusion
SpecificationsAMS 4336
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.5.0, Table 3.7.5.0(c) (pdf page 365 of the chapter file)
Dimension bands2
Density2851 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 band0.000–0.249 in (0–6.325 mm)0.250–0.499 in (6.35–12.67 mm)
SpecificationAMS 4336AMS 4336
BasisABAB
Ftu, MPaL613.6627.4620.5648.1
LT572.3586.1579.2599.8
Fty, MPaL586.1599.8586.1627.4
LT544.7558.5544.7586.1
Fcy, MPaL579.2592.9586.1627.4
LT592.9606.7592.9634.3
Fsu, MPaL317.2324.1324.1337.8
LT317.2324.1324.1337.8
Fbru (e/D = 1.5), MPaL841.2861.8854.9889.4
LT841.2861.8854.9889.4
Fbru (e/D = 2.0), MPaL1103112411101165
LT1103112411101165
Fbry (e/D = 1.5), MPaL723.9737.7723.9772.2
LT723.9737.7723.9772.2
Fbry (e/D = 2.0), MPaL854.9875.6854.9910.1
LT854.9875.6854.9910.1
e, %L7999
LT…………
E, GPa71.7171.7171.7171.71
Ec, GPa74.4674.4674.4674.46
G, GPa26.8926.8926.8926.89
ν0.330.330.330.33
ρ, kg/m³2851285128512851

Effect of Temperature

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

Other 7055 Tables

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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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