Residual Strength in the Presence of Fatigue Cracks

Abstract

The results are presented of an AGARD project - 'To review the existing state of knowledge with respect to the residual strength of material specimens containing fatigue crack failure initiation of known proportions; and to ascertain the present knowledge existing with respect to the residual strength of typical structures using various types of materials.' The report concentrates on the critical analysis of methods of calculation useful in practice, rather than the presentation of a comprehensive summary.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1967
Accession Number
AD0669772

Entities

People

  • Paul Kuhn

Organizations

  • AGARD

Tags

Communities of Interest

  • Air Platforms
  • Space

DTIC Thesaurus Topics

  • Aircraft Industry
  • Aircrafts
  • Aluminum Alloys
  • Engineering
  • Engineers
  • Ferrium
  • Fracture (Mechanics)
  • Materials
  • Materials Engineering
  • Materials Testing
  • Mechanics
  • Military Aircraft
  • Notch Toughness
  • Stress Concentration
  • Stress Strain Relations
  • Structural Engineering
  • Tensile Strength

Fields of Study

  • Materials science

Readers

  • Materials Science (Mechanical Engineering).
  • Systems Analysis and Design