Fatigue characteristics of a notched specimen made of commercially-pure titanium

Shigeru Hamada, Hiroshi Noguchi

研究成果: Contribution to journalArticle査読

1 被引用数 (Scopus)

抄録

This study aimed to clarify the implication of the stress amplitude of the no failure state at N = 107 cycles for commercially-pure titanium and the influence of the strain age hardening of commercially-pure titanium on the fatigue characteristics. To this end, rotating bending fatigue tests on smooth and notched specimens made of commercially-pure titanium were performed. After removing the oxygen solution layer of the specimen, a proportional relationship was noted between the maximum stress at the notch root and logarithm of the number of cycles to the fatigue crack initiation. In addition, it was observed that if only one type of fatigue crack initiates from the notch root and internal fracture does not occur, the fatigue limit is the stress amplitude at which a fatigue crack does not initiate at N = 107 cycles. After 2 × 108 cycles, the strain age hardening does not considerably influence the fatigue characteristics of commercially-pure titanium.

本文言語英語
論文番号102764
ジャーナルTheoretical and Applied Fracture Mechanics
109
DOI
出版ステータス出版済み - 10 2020

All Science Journal Classification (ASJC) codes

  • 材料科学(全般)
  • 凝縮系物理学
  • 機械工学
  • 応用数学

フィンガープリント

「Fatigue characteristics of a notched specimen made of commercially-pure titanium」の研究トピックを掘り下げます。これらがまとまってユニークなフィンガープリントを構成します。

引用スタイル