Strain-Rate Sensitivity of Three Titanium-Alloy Sheet Materials After Prolonged Exposure AT 550 degree F (561 degree K)

Abstract

Results are presented of an investigation on the effects of strain rate on three titanium-alloy sheet materials before and after prolonged exposure without stress at 550 degrees F (561 degrees K). The strain-rate sensitivity of the three alloys, Ti-8Al-lMo-1V, Ti-4Al-3Mo-1V, and Ti-6Al-4V, was determined from the results of tensile tests performed at three strain rates on smooth and V-notched specimens.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1969
Accession Number
ADA379805

Entities

People

  • Robert M. Baucom

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Alloys
  • Materials
  • Mechanical Properties
  • Recording Systems
  • Strain Gages
  • Strain Rate
  • Stress Strain Relations
  • Stresses
  • Supersonic Aircraft
  • Supersonic Transport Aircraft
  • Tensile Properties
  • Tensile Strength
  • Tensile Testing
  • Titanium
  • Titanium Alloys
  • Water
  • Yield Strength

Fields of Study

  • Materials science

Readers

  • Mechanical Engineering/Mechanics of Materials.
  • Metallurgy
  • Nuclear and Radiation Engineering.