Tools › Materials › Aluminum › 2024-T42 Clad flat sheet and plate

2024-T42 Clad flat sheet and plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2024 / T42 / Clad flat sheet and plate
SpecificationsAMS-QQ-A-250/5
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.3.0, Table 3.2.3.0(e) (pdf page 77 of the chapter file)
Dimension bands7
Density0.1 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 band0.008–0.009 in0.010–0.062 in0.063–0.249 in0.250–0.499 in0.500–1.000 in1.001–2.000 in2.001–3.000 in
SpecificationAMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5AMS-QQ-A-250/5
BasisABABABSSS
Ftu, ksiL555757596062605958
Fty, ksiL343534353638363636
Fcy, ksiL383938394042393835
Fsu, ksiL333434353637363535
Fbru (e/D = 1.5), ksiL889191949699959083
Fbru (e/D = 2.0), ksiL109113113117119123119117115
Fbry (e/D = 1.5), ksiL606160616367636363
Fbry (e/D = 2.0), ksiL727472747680767676
E, Msi10.510.510.510.510.510.510.710.710.7
Ec, Msi10.710.710.710.710.710.710.910.910.9
ν0.330.330.330.330.330.330.330.330.33
ρ, lb/in30.10.10.10.10.10.10.10.10.1

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_ty
10099.4100
20095.898
30088.995
40071.484
50037.947.6
60020.322.8
70011.812.9

Factors in percent of the room-temperature allowable.

Other 2024 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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.