Heat-Resistant Alloys for Ordnance Materiel and Aircraft and Naval Engine Parts (N-102): Part 2 - Cobalt and Nickel in 26% Cr Alloys

Abstract

In the investigation of heat-resisting alloys, the effects of nickel and cobalt have been studied in two groups of 26% Cr alloys, one series being essentially nonferrous and the other containing about 50% iron. The results of stress-strain-rupture tests at 1600 and 1800 deg F are given. Data from room temperature tension tests are included for materials as cast or after exposure to one of several aging treatments. In the absence of iron, the replacement of nickel by cobalt produces a marked strengthening at elevated temperatures. Creep testing of several compositions has been initiated to supplement the indications of stress-strain-rupture tests; two tests at 1800 deg F having been completed for this report. The microstructures of these alloys have been examined, and representative photomicrographs are shown.

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Document Details

Document Type
Technical Report
Publication Date
Jul 12, 1945
Accession Number
ADA801486

Entities

People

  • Earnshaw Cook
  • F. S. Gardner
  • Howard S. Avery

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Force
  • Aircrafts
  • Alloys
  • Castings
  • Chemical Analysis
  • Chemical Elements
  • Chemistry
  • Corrosion Resistance
  • Creep Tests
  • Heat Resistant Alloys
  • High Temperature
  • Materials
  • Metallurgy
  • Munitions
  • National Security
  • Navy
  • Solid Solutions

Fields of Study

  • Materials science

Readers

  • Materials Science and Engineering.
  • Metallurgy