Fatigue crack growth and delamination behaviours of advanced Al-Li alloy laminate under single tensile overload

著录项

• 来源
  《Fatigue & fracture of engineering materials and structures》 |2016年第1期|47-56|共10页
• 作者

  Y. HUANG; J. Z. LIU; X. HUANG; J. Z. ZHANG; G. Q. YUE;

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• 作者单位

  Beijing Institute of Aeronautical Materials, Beijing 100095, China;

  Beijing Institute of Aeronautical Materials, Beijing 100095, China;

  Beijing Institute of Aeronautical Materials, Beijing 100095, China;

  Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, China;

  Beijing Aeronautical Science & Technology Research Institute of COMAC, Beijing 102211, China;

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• 收录信息
• 原文格式 PDF
• 正文语种 eng
• 中图分类
• 关键词

  Al-Li alloy laminate; crack growth; delamination; fatigue; single overload;

  机译：铝锂合金层压板裂纹增长分层疲劳;单重载;