DESIGN INFORMATION ON NICKEL-BASE ALLOYS FOR AIRCRAFT AND MISSILES

摘要

Tensile, compressive, shear, and bearing properties of some nickel-base alloys for aircraft and missiles have been assembled and evaluated. Tentative design curves showing the effect of temperature on these proper?ties are presented in a format consistent with the design document, MIL.-HDBK-5 (superseding ANC-5) Strength of Metal Aircraft Elements. These data will be reviewed in October, 1960, by the ANC-5 Panel before the de?sign curves, or modifications of them, can be included in MIL.-HDBK-5.nIn addition to the mechanical-property data, background information on these alloys is presented to aid in the selection of alloys for given elevated-temperature applications.