Tools › Materials › Aluminum › 6013-T6 Sheet

6013-T6 Sheet: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form6013 / T6 / Sheet
SpecificationsAMS 4216 and AMS 4347
HandbookMIL-HDBK-5J, 31 January 2003, section 3.6.1.0, Table 3.6.1.0(b) (pdf page 259 of the chapter file)
Dimension bands3
Density0.098 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 band0.010–0.062 in0.063–0.125 in0.126–0.249 in
SpecificationAMS 4216 and AMS 4347AMS 4216 and AMS 4347AMS 4216 and AMS 4347
BasisSSS
Ftu, ksiL525252
LT525252
Fty, ksiL474748
LT464646
Fcy, ksiL484848
LT484849
Fsu, ksiL323232
LT323232
Fbru (e/D = 1.5), ksiL858585
LT858585
Fbru (e/D = 2.0), ksiL111111111
LT111111111
Fbry (e/D = 1.5), ksiL666971
LT666971
Fbry (e/D = 2.0), ksiL768082
LT768082
e, %L………
LT888
E, Msi9.99.99.9
Ec, Msi10.110.110.1
G, Msi3.83.83.8
ρ, lb/in30.0980.0980.098

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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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