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2124-T851 Plate: MIL-HDBK-5J Design Allowables

Material classAluminum
Alloy / temper / form2124 / T851 / Plate
SpecificationsAMS 4101 and AMS-QQ-A-250/29
HandbookMIL-HDBK-5J, 31 January 2003, section 3.2.7.0, Table 3.2.7.0(b) (pdf page 158 of the chapter file)
Dimension bands6
Density2768 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 band1.000–1.500 in (25.4–38.1 mm)1.501–2.000 in (38.13–50.8 mm)2.001–3.000 in (50.83–76.2 mm)3.001–4.000 in (76.23–101.6 mm)4.001–5.000 in (101.6–127 mm)5.001–6.000 in (127–152.4 mm)
SpecificationAMS 4101 and AMS-QQ-A-250/29AMS 4101 and AMS-QQ-A-250/29AMS 4101 and AMS-QQ-A-250/29AMS 4101 and AMS-QQ-A-250/29AMS 4101 and AMS-QQ-A-250/29AMS 4101 and AMS-QQ-A-250/29
BasisSABABABABAB
Ftu, MPaL455.1455.1468.8448.2468.8448.2461.9441.3455.1434.4448.2
LT455.1455.1468.8448.2468.8448.2461.9441.3455.1434.4448.2
ST441.3441.3455.1434.4441.3427.5434.4420.6427.5399.9406.8
Fty, MPaL393393420.6393420.6386.1413.7379.2399.9372.3386.1
LT393393420.6393420.6386.1413.7379.2399.9372.3386.1
ST379.2379.2406.8379.2406.8372.3393365.4379.2351.6365.4
Fcy, MPaL393393420.6386.1413.7379.2406.8365.4386.1358.5372.3
LT393393420.6393420.6386.1413.7379.2399.9372.3386.1
ST…393420.6399.9427.5393420.6393413.7386.1399.9
Fbru (e/D = 1.5), MPaL…668.8689.5661.9689.5661.9682.6648.1668.8641.2661.9
LT…668.8689.5661.9689.5661.9682.6648.1668.8641.2661.9
ST…668.8689.5661.9689.5661.9682.6648.1668.8641.2661.9
Fbru (e/D = 2.0), MPaL…868.7896.3861.8896.3861.8882.5848.1868.7834.3861.8
LT…868.7896.3861.8896.3861.8882.5848.1868.7834.3861.8
ST…868.7896.3861.8896.3861.8882.5848.1868.7834.3861.8
Fbry (e/D = 1.5), MPaL…544.7579.2551.6586.1551.6586.1544.7579.2544.7565.4
LT…544.7579.2551.6586.1551.6586.1544.7579.2544.7565.4
ST…544.7579.2551.6586.1551.6586.1544.7579.2544.7565.4
Fbry (e/D = 2.0), MPaL…627.4675.7634.3682.6634.3682.6634.3668.8627.4655
LT…627.4675.7634.3682.6634.3682.6634.3668.8627.4655
ST…627.4675.7634.3682.6634.3682.6634.3668.8627.4655
e, %L66666555555
LT55544444444
ST1.51.51.51.51.51.51.51.51.51.51.5
E, GPa71.7171.7171.7171.7171.7171.7171.7171.7171.7171.7171.71
Ec, GPa75.1575.1575.1575.1575.1575.1575.1575.1575.1575.1575.15
G, GPa27.5827.5827.5827.5827.5827.5827.5827.5827.5827.5827.58
ν0.330.330.330.330.330.330.330.330.330.330.33
ρ, kg/m³27682768276827682768276827682768276827682768

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
3898.898.3
9392.192.2
14982.984.3
20470.8

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.