跳到主要导航 跳到搜索 跳到主要内容

Study on compressive properties of stitched laminates

  • Gang Chen*
  • , Zheng Neng Li
  • , Xiao Quan Cheng
  • , Chang He Kou
  • *此作品的通讯作者
  • Beihang University

科研成果: 期刊稿件文章同行评审

摘要

Experimental investigation is conducted to understand the compression strength and failure mechanisms of stitched laminates and unstitched laminates. A finite element method is adopted to calculate the effects of stitch parameters on the compressive properties of the stitched. Results show that the critical damage event in the stitched laminates is kink band formation, and that the delamination is suppressed. The stitching parameters have effects on the are compression strength. The results determined by this method are correlated well with the test results.

源语言英语
页(从-至)444-447
页数4
期刊Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica
27
3
出版状态已出版 - 5月 2006

指纹

探究 'Study on compressive properties of stitched laminates' 的科研主题。它们共同构成独一无二的指纹。

引用此