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AISI 4130-Normalized and tempered, stress relieved Sheet, strip, plate, / bars, and forgings: MIL-HDBK-5J Design Allowables

Material classSteel
Alloy / temper / formAISI 4130 / Normalized and tempered, stress relieved / Sheet, strip, plate, / bars, and forgings
SpecificationsAMS 6350 / AMS 6528 / AMS-S-6758
HandbookMIL-HDBK-5J, 31 January 2003, section 2.3.1.0, Table 2.3.1.0(g) (pdf page 24 of the chapter file)
Dimension bands2
Density0.283 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 band0.000–0.188 in0.188– in
SpecificationAMS 6350 / AMS 6528 / AMS-S-6758AMS 6350 / AMS 6528 / AMS-S-6758
BasisSS
Ftu, ksi9590
Fty, ksi7570
Fcy, ksi7570
Fsu, ksi5754
Fbru (e/D = 2.0), ksi200190
Fbry (e/D = 2.0), ksi129120
E, Msi2929
Ec, Msi2929
G, Msi1111
ν0.320.32
nt (Ramberg-Osgood)8…
nc (Ramberg-Osgood)10…
ρ, lb/in30.2830.283

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

°FF_tuF_tyF_cyF_suF_bruF_bry
-100105.2106.7
0101.3102.8
10099.298.898.699.599.899.3
20098.194.891.197.397.496.6
30096.790.886.796.296.595.5
40095.186.983.895.596.194.3
50092.482.981.594.295.493.8
60088.978.978.691.691.491.7
70083.474.47486.583.786.9
80076.968.465.777.474.577.9
10005842.656.254.256.9
120035.223.137.2

Factors in percent of the room-temperature allowable.

Stress-Strain Curves (Ramberg-Osgood)

ε = σ/E + 0.002 (σ/F_y)^n with the first band's S-basis yield strength and the exponent on file for it (the tension curve stops at F_tu).

Ramberg-Osgood design stress-strain curves at room temperature

Other AISI 4130 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.