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Abstract <p>The peeling of a coating in a two-layer composite is studied. Formulas for the critical number of loading cycles are determined. Beyond that number, normal rupture stress results in failure of the adhesive and peeling of the coating.</p>

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Fatigue Failure of Composites

  • 期刊论文

  • 发表日期：

    2025年4月1日

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  • I. K. Arkhipov,
  • S. I. Koryagin,
  • V. I. Abramova,
  • N. H. Sagatelyan,
  • P. R. Grishin

摘要

Abstract

The peeling of a coating in a two-layer composite is studied. Formulas for the critical number of loading cycles are determined. Beyond that number, normal rupture stress results in failure of the adhesive and peeling of the coating.