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7075-T651 Clad plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7075 / T651 / Clad plate
SpecificationsAMS 4049 and AMS-QQ-A-250/13
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.6.0, Table 3.7.6.0(c) (pdf page 377 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 4049 and AMS-QQ-A-250/13AMS 4049 and AMS-QQ-A-250/13AMS 4049 and AMS-QQ-A-250/13AMS 4049 and AMS-QQ-A-250/13AMS 4049 and AMS-QQ-A-250/13AMS 4049 and AMS-QQ-A-250/13AMS 4049 and AMS-QQ-A-250/13
BasisABABABABABABAB
Ftu, ksiL7476757774767375697168706466
LT7577767875777476707269716567
ST………………7071666865676163
Fty, ksiL6769687067696466616358605456
LT6567666865676264596156585254
ST………………5961565854555052
Fcy, ksiL6567666864666062575853554951
LT6971707269716568626459615557
ST………………6770646661635759
Fsu, ksiL4243424442444344414240423839
LT4243424442444344414240423839
ST………………4344414240423839
Fbru (e/D = 1.5), ksiL11311611411711311611111410510810410798101
LT11311611411711311611111410510810410798101
ST………………11111410510810410798101
Fbru (e/D = 2.0), ksiL139143141145139143137141130134128132121124
LT139143141145139143137141130134128132121124
ST………………137141130134128132121124
Fbry (e/D = 1.5), ksiL949797100971009598909486898084
LT949797100971009598909486898084
ST………………9598909486898084
Fbry (e/D = 2.0), ksiL1111141131161131171101131051091001049397
LT1111141131161131171101131051091001049397
ST………………1101131051091001049397
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
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.