High Temperature Cyclic Behaviour of Aerospace Materials: Room Temperature Validation Tests of Ti-6Al-4V,

Abstract

Materials specification and distribution of Ti-6A1-4V specimens are presented along with the collated data from those participants that have supplied test results. Crack propagation and strain control low cycle fatigue data are discussed, along with a number of points of clarification regarding test technique. jg

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1994
Accession Number
ADA294413

Entities

People

  • C. R. Gostelow
  • C. Wilkinson

Organizations

  • AGARD

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Air Force
  • Crack Propagation
  • Cracks
  • Data Analysis
  • Databases
  • Fatigue Tests (Mechanics)
  • Gages
  • High Temperature
  • Materials
  • Measurement
  • Measuring Instruments
  • Modulus Of Elasticity
  • Nato
  • Stress Strain Relations
  • Stresses
  • Test Methods
  • United States

Readers

  • Materials Science (Mechanical Engineering).
  • Powder metallurgy of Titanium alloys.
  • Systems Analysis and Design

Technology Areas

  • Space