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Optimized design of composite skin-stiffened structure with large cutout

  • Chu Yang Luo*
  • , Jun Jiang Xiong
  • , Xiao Su Yi
  • , Zi Long Zhang
  • , Gang Liu
  • *此作品的通讯作者
  • Beihang University
  • Beijing Institute of Aeronautical Materials

科研成果: 期刊稿件文章同行评审

摘要

The optimized design of composite skin-stiffened structure with large cutout was conducted by finite element method. The effect of cutout reinforcement and stiffened reinforcement to the buckling load was investigated. The results show that stress concentration is far away from the free edge of hole after flanged reinforcement. The buckling load enhances with increasing both flanged depth and width. The co-cure stiffened is better than integral stiffened. At coordinative condition, the low and dense stiffener is recommended, as well as increasing transverse stiffeners.

源语言英语
页(从-至)9-13
页数5
期刊Journal of Materials Engineering
4
出版状态已出版 - 4月 2011

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