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7075-T651 Plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7075 / T651 / Plate
SpecificationsAMS 4045 and AMS-QQ-A-250/12
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(b) (pdf page 371 of the chapter file)
Dimension bands7
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 band0.250–0.499 in0.500–1.000 in1.001–2.000 in2.001–2.500 in2.501–3.000 in3.001–3.500 in3.501–4.000 in
SpecificationAMS 4045 and AMS-QQ-A-250/12AMS 4045 and AMS-QQ-A-250/12AMS 4045 and AMS-QQ-A-250/12AMS 4045 and AMS-QQ-A-250/12AMS 4045 and AMS-QQ-A-250/12AMS 4045 and AMS-QQ-A-250/12AMS 4045 and AMS-QQ-A-250/12
BasisABABABABABABAB
Ftu, ksiL7779777976787577717370726668
LT7880788077797678727471736769
ST………………7071666865676163
Fty, ksiL6971707269716668636560625658
LT6769687067696466616358605456
ST………………5961565854555052
Fcy, ksiL6769687066686264586055575152
LT7173727471736870656761645759
ST………………6770646661635759
Fsu, ksiL4344444544454445424342433941
LT4344444544454445424342433941
ST………………4445424342433941
Fbru (e/D = 1.5), ksiL117120117120116119114117108111107110101104
LT117120117120116119114117108111107110101104
ST………………114117108111107110101104
Fbru (e/D = 2.0), ksiL145148145148143147141145134137132135124128
LT145148145148143147141145134137132135124128
ST………………141145134137132135124128
Fbry (e/D = 1.5), ksiL9710010010310010398101949789938487
LT9710010010310010398101949789938487
ST………………98101949789938487
Fbry (e/D = 2.0), ksiL11411811712011712011311710911210410898103
LT11411811712011712011311710911210410898103
ST………………11311710911210410898103
e, %L……………………………………
LT99776655555533
ST……………………………………
E, Msi10.310.310.310.310.310.310.310.310.310.310.310.310.310.3
Ec, Msi10.610.610.610.610.610.610.610.610.610.610.610.610.610.6
G, Msi3.93.93.93.93.93.93.93.93.93.93.93.93.93.9
ν0.330.330.330.330.330.330.330.330.330.330.330.330.330.33
ρ, lb/in30.1010.1010.1010.1010.1010.1010.1010.1010.1010.1010.1010.1010.1010.101

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
-300117.8117.6
-200110110
-100105.5105.6
0102.9102.8
10098.698.999.899.897.299.5
20089.291.294.79787.596.1
30074.27980.584.677.884.3
40045.75050.558.253.158.5
50019.919.820.227.724.323.1
60011.811.815.614.5

Factors in percent of the room-temperature allowable.

Other 7075 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.