Tensile, Fatigue, and Creep Properties of Forged Aluminum Alloys at Temperatures Up to 800 deg. F

Abstract

This paper presents data on the tensile strength, fatigue strength, creep properties, and thermal expansion of forged aluminum alloys XBl8S, 185, 24S, and 325, which are pertinent to the application of these alloys in the temperature range from 700 to 8Q%O F. Included arc data taken from published sources, unpublished material made available through the courtesy of the Aluminum Company of America and the National Bureau of Standards, and original data, obtained at Battelle Memorial Institute, which extend this previous information. The work also contains a critical discussion of the data and their application to design of aircraft engine.

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Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1948
Accession Number
ADA380901

Entities

People

  • H. C. Cross
  • J. M. Berry
  • L. R. Jackson

Organizations

  • Battelle Memorial Institute

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aluminum Alloys
  • Creep
  • Creep Tests
  • Fabrication
  • Fatigue Tests (Mechanics)
  • Grain Size
  • High Temperature
  • Materials
  • Mechanical Properties
  • Mechanical Working
  • Stresses
  • Temperature Gradients
  • Tensile Properties
  • Tensile Strength
  • Thermal Expansion
  • Universal Joints
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Powder metallurgy of Titanium alloys.
  • Seismology
  • Technical Research and Report Writing.