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7010-T7451 Plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7010 / T7451 / Plate
SpecificationsAMS 4205
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.1.0, Table 3.7.1.0(b) (pdf page 295 of the chapter file)
Dimension bands6
Density0.102 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 band0.250–1.000 in1.001–2.000 in2.001–3.000 in3.001–4.000 in4.001–5.000 in5.001–6.000 in
SpecificationAMS 4205AMS 4205AMS 4205AMS 4205AMS 4205AMS 4205
BasisSSABABABAB
Ftu, ksiL71717072707168716870
LT72727172707269716771
ST……6668666865676367
Fty, ksiL62626062606259615761
LT62626062596158605760
ST……5557545653555254
Fcy, ksiL61615961586057595659
LT63636264616360625963
ST……6163606259615861
Fsu, ksiL41414242424342434143
LT41414242424342434143
ST……4242424342434143
Fbru (e/D = 1.5), ksiL10010110110210010310010397103
LT10010110110210010310010397103
ST……10110210010310010397103
Fbru (e/D = 2.0), ksiL127129130132130134129133126133
LT127129130132130134129133126133
ST……130132130134129133126133
Fbry (e/D = 1.5), ksiL81828184818481848084
LT81828184818481848084
ST……8184818481848084
Fbry (e/D = 2.0), ksiL949797100981019810197102
LT949797100981019810197102
ST……97100981019810197102
e, %L9999999988
LT6666665555
ST……2.52.5222222
E, Msi10.210.210.210.210.210.210.210.210.210.2
Ec, Msi10.610.610.610.610.610.610.610.610.610.6
G, Msi3.93.93.93.93.93.93.93.93.93.9
ν0.330.330.330.330.330.330.330.330.330.33
ρ, lb/in30.1020.1020.1020.1020.1020.1020.1020.1020.1020.102

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

°FF_tuF_ty
10097.299.5
20085.392.8
30072.580.2

Factors in percent of the room-temperature allowable.

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.