Effect of Interspersed Periods of Heating on Fatigue Crack Initiation and Propagation in CM001 (RR58) Clad Sheet.

Abstract

Fatigue tests have been conducted to study the effect of interspersed periods of heating on the initiation and early growth of cracks from holes in clad sheet and also on later stages of crack propagation. The tests were under flight simulation loading and the material was CM001 (RR58) clad aluminium alloy sheet. Interspersed heating reduced the lives to initiate and grow cracks to 2mm and this is attributed to the softening of strain hardened material at the crack tip, but no effect was observed for longer crack lengths. When load was applied during the periods of heating creep redistribution of local stress retarded the growth of short and long cracks. Further work is underway to investigate fatigue-heat interactions under different load-temperature sequences, other forms of material, and over a wider range of crack lengths. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1976
Accession Number
ADA041014

Entities

People

  • F. E. Kiddle

Tags

Communities of Interest

  • Air Platforms
  • Counter IED
  • Sensors

DTIC Thesaurus Topics

  • Aircrafts
  • Aluminum
  • Aluminum Alloys
  • Chemical Composition
  • Crack Propagation
  • Crack Tips
  • Cracks
  • Creep
  • Creep Tests
  • Fatigue Tests (Mechanics)
  • Hydraulic Jacks
  • Materials
  • Measurement
  • Stresses
  • Supersonic Transport Aircraft
  • Tensile Properties
  • Tensile Strength

Fields of Study

  • Materials science

Readers

  • Materials Science (Mechanical Engineering).
  • Materials Science and Engineering.