Tools › Materials › Heat-Resistant › L-605-Solution treated Sheet

L-605-Solution treated Sheet: MIL-HDBK-5J Design Allowables

Material classHeat-Resistant
Alloy / temper / formL-605 / Solution treated / Sheet
SpecificationsAMS 5537
HandbookMIL-HDBK-5J, 31 January 2003, section 6.4.1.0, Table 6.4.1.0(b) (pdf page 118 of the chapter file)
Dimension bands1

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 band0.010–0.187 in (0.254–4.75 mm)
SpecificationAMS 5537
BasisAB
Ftu, MPaL868.7903.2
LT896.3930.8
Fty, MPaL393427.5
LT379.2413.7
Fcy, MPaL282.7310.3
LT386.1420.6
Fsu, MPaL627.4655
LT627.4655
Fbru (e/D = 1.5), MPaL12821331
LT12821331
Fbru (e/D = 2.0), MPaL16001662
LT16001662
Fbry (e/D = 1.5), MPaL606.7661.9
LT606.7661.9
Fbry (e/D = 2.0), MPaL779.1848.1
LT779.1848.1
E, GPa224.8224.8
Ec, GPa224.8224.8
G, GPa86.8786.87
ν0.290.29

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

°CF_tuF_tyF_cyF_suF_bruF_bry
3899.79996.899.699.197.3
9396.18985.298.696.182.6
14992.579.976.297.293.975
2048971.169.495.891.772.1
2685.46365.693.789.869.8
31682.457.863.990.487.968
37180.15663.485.284.666.6
42777.955.363.179.881.165.3
53872.453.761.568.871.163.9
64964.851.758.458.258.662.1

Factors in percent of the room-temperature allowable.

Other L-605 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from the chapter tables; check the printed table before use in a certified analysis, and note that MIL-HDBK-5J was superseded by MMPDS, whose later editions may differ.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.