Accession Number : AD0286532

Title :   EVALUATION OF TYPE H-11 (5-CHROME) STEEL AT HIGH STRENGTH LEVELS

Corporate Author : NAVAL AIR ENGINEERING CENTER PHILADELPHIA PA AERONAUTICAL MATERIALS LAB

Personal Author(s) : VIGLIONE,J.

Report Date : 06 AUG 1962

Pagination or Media Count : 1

Abstract : Test results show that air quenched Halcomb 218 sheet ma erial te pered at t p ratures ranging between 1050 and 115 F gav pproxi a ly e u l values for net fracture stre g h, and for cr ck e nsion force. (Author)

Descriptors :   *CHROMIUM ALLOYS, *FRACTURE (MECHANICS), *STEEL, ALLOYS, HEAT TREATMENT

Distribution Statement : APPROVED FOR PUBLIC RELEASE