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2014-T6, T6510, and T6511 Extruded bar, rod, and shapes: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2014 / T6, T6510, and T6511 / Extruded bar, rod, and shapes
SpecificationsAMS 4153 and AMS-QQ-A-200/2
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.1.0, Table 3.2.1.0(g) (pdf page 35 of the chapter file)
Dimension bands8
Density0.101 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 band0.000–0.749 in0.000–0.750 in, area 25–32 in20.125–0.499 in, area 0–25 in20.500–0.749 in, area 0–25 in20.750–1.499 in, area 0–25 in21.500–1.750 in, area 0–25 in21.751–2.999 in, area 0–25 in23.000–4.499 in, area 0–25 in2
SpecificationAMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2AMS 4153 and AMS-QQ-A-200/2
BasisSSABABABABSS
Ftu, ksiL606860626468687068716868
LT…5660…64…63…61…6158
Fty, ksiL535853575862606360636060
LT…4753…55…54…52…5249
Fcy, ksiL……5256576159625962……
LT………………………………
Fsu, ksiL……3536373939413941……
LT……35…37…39…39………
Fbru (e/D = 1.5), ksiL……909396102102105102106……
LT……90…96…102…102………
Fbru (e/D = 2.0), ksiL……116120124132132136132138……
LT……116…124…132…132………
Fbry (e/D = 1.5), ksiL……7378808582868286……
LT……73…80…82…82………
Fbry (e/D = 2.0), ksiL……859193999610196101……
LT……85…93…96…96………
e, %L677777777…77
LT…15…5…5…2…21
E, Msi10.810.810.810.810.810.810.810.810.810.810.810.8
Ec, Msi111111111111111111111111
G, Msi4.14.14.14.14.14.14.14.14.14.14.14.1
ν0.330.330.330.330.330.330.330.330.330.330.330.33
ρ, lb/in30.1010.1010.1010.1010.1010.1010.1010.1010.1010.1010.1010.101

Effect of Temperature

Percent of the room-temperature value against temperature, digitized from the handbook figures (the shortest exposure of each figure, every 10 °F). Strength curves give the allowable at temperature; "after exposure" curves give the room-temperature property after a soak at that temperature.

Strength allowables at temperature, percent of room temperature

Moduli at temperature

Elongation and exposure effects

°FF_tuF_tyF_cyF_suF_bruF_bry
-300112.5113.2
-200106.5108.8
-100103.6105.3
0101.5102.1
10098.89998.699.299.199
20093.395.191.894.594.794.6
30084.386.582.986.986.787.7
40068.468.267.373.170.173.4
50034.936.231.850.935.134.9
60014.615.315.823.321.721.3
7008.17.611.212.813.212.8
8004.9

Factors in percent of the room-temperature allowable.

Other 2014 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.