Fatigue crack growth of bonded composite repairs in gigacycle regime

Q. Y. Wang, M. R. Sriraman, N. Kawagoishi, Q. Chen

研究成果: ジャーナルへの寄稿学術誌査読

14 被引用数 (Scopus)

抄録

Fatigue induced from various aeromechanical sources can reach gigacycle regime due to vibratory stress cycles at high frequencies. Composite repairs offer various advantages over mechanical fastening or riveting, including improved long-term durability behavior and reduced corrosion. In this study, by using ultrasonic frequency cyclic loading, fatigue crack growth tests in gigacycle regime were conducted on notched 7075 and 6061 aluminum alloy substrates (in T6 condition) with and without bonded Boron/epoxy patches. A considerable increase in the fatigue life was observed with more number of patch plies. The effect of patch configuration and thickness on enhancing the fatigue strength by orders of magnitude has been demonstrated.

本文言語英語
ページ(範囲)1197-1201
ページ数5
ジャーナルInternational Journal of Fatigue
28
10 SPEC. ISS.
DOI
出版ステータス出版済み - 10月 2006
外部発表はい

!!!All Science Journal Classification (ASJC) codes

  • モデリングとシミュレーション
  • 材料科学(全般)
  • 材料力学
  • 機械工学
  • 産業および生産工学

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