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7040-T7451 Plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form7040 / T7451 / Plate
SpecificationsAMS 4211
HandbookMIL-HDBK-5J, 31 January 2003, section 3.7.2.0, Table 3.7.2.0(b) (pdf page 303 of the chapter file)
Dimension bands6
Density2823 kg/m³

Design Mechanical and Physical Properties (room temperature)

Converted from the handbook table (ksi, Msi, lb/in³) and rounded to 4 significant figures; dimension bands in inches with mm in parentheses. 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 band3.001–4.000 in (76.23–101.6 mm)4.001–5.000 in (101.6–127 mm)5.001–6.000 in (127–152.4 mm)6.001–7.000 in (152.4–177.8 mm)7.001–8.000 in (177.8–203.2 mm)8.001–8.500 in (203.2–215.9 mm)
SpecificationAMS 4211AMS 4211AMS 4211AMS 4211AMS 4211AMS 4211
BasisABABABABABAB
Ftu, MPaL496.4496.4489.5496.4482.6489.5475.7482.6468.8482.6468.8482.6
LT496.4510.2489.5503.3482.6496.4475.7482.6468.8475.7468.8475.7
ST475.7482.6468.8482.6468.8475.7455.1461.9455.1461.9455.1461.9
Fty, MPaL427.5448.2427.5441.3427.5441.3427.5427.5420.6427.5420.6434.4
LT427.5448.2427.5448.2420.6434.4413.7427.5413.7420.6406.8420.6
ST406.8420.6399.9420.6399.9420.6393399.9393399.9386.1399.9
Fcy, MPaL413.7434.4413.7427.5406.8420.6399.9413.7406.8413.7406.8420.6
LT441.3461.9441.3461.9434.4455.1427.5441.3427.5441.3420.6434.4
ST434.4455.1434.4455.1427.5448.2420.6434.4420.6434.4413.7434.4
Fsu, MPaL310.3324.1303.4317.2303.4310.3296.5303.4296.5303.4296.5303.4
LT310.3324.1303.4317.2303.4310.3296.5303.4296.5303.4296.5303.4
ST310.3324.1303.4317.2303.4310.3296.5303.4296.5303.4296.5303.4
Fbru (e/D = 1.5), MPaL786806.7772.2792.9758.4786744.6758.4723.9744.6723.9730.8
LT786806.7772.2792.9758.4786744.6758.4723.9744.6723.9730.8
ST786806.7772.2792.9758.4786744.6758.4723.9744.6723.9730.8
Fbru (e/D = 2.0), MPaL999.710349861014965.3999.7944.6965.3923.9937.7917923.9
LT999.710349861014965.3999.7944.6965.3923.9937.7917923.9
ST999.710349861014965.3999.7944.6965.3923.9937.7917923.9
Fbry (e/D = 1.5), MPaL641.2668.8641.2668.8634.3661.9620.5641.2620.5634.3606.7627.4
LT641.2668.8641.2668.8634.3661.9620.5641.2620.5634.3606.7627.4
ST641.2668.8641.2668.8634.3661.9620.5641.2620.5634.3606.7627.4
Fbry (e/D = 2.0), MPaL786820.5786820.5772.2806.7758.4779.1758.4779.1744.6772.2
LT786820.5786820.5772.2806.7758.4779.1758.4779.1744.6772.2
ST786820.5786820.5772.2806.7758.4779.1758.4779.1744.6772.2
e, %L9999887…6…6…
LT6655444…4…4…
ST3333333…3…3…
E, GPa71.7171.7171.7171.7171.7171.7171.7171.7171.7171.7171.7171.71
Ec, GPa73.0873.0873.0873.0873.0873.0873.0873.0873.0873.0873.0873.08
G, GPa26.8926.8926.8926.8926.8926.8926.8926.8926.8926.8926.8926.89
ν0.330.330.330.330.330.330.330.330.330.330.330.33
ρ, kg/m³282328232823282328232823282328232823282328232823

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

°CF_tuF_ty
-18104.2103.2
3897.598.2
9387.991.3
14975.882.3

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.