Effects of ply orientation on nonlinear buckling of Aircraft composite stiffened panel
作者: OuadiaAbdelmajidAhmedMohamed
作者单位: 1Faculty of Technology, University Djillali Liabes, Sidi bel Abbes, Algeria.
2Laboratoire�RTFM, Ecole Nationale Polytechnique Maurice Audin, Oran,�Algeria.
3Laboratoire LMPM, University Djillali Liabes, Sidi bel Abbes, Algeria.
4Laboratoire LABAB, Ecole Nationale Polytechnique Maurice Audin, Oran, Algeria.
刊名: Fracture and Structural Integrity, 2019, Vol.13 (50), pp.126 - 140
来源数据库: Gruppo Italiano Frattura
DOI: 10.3221/IGF-ESIS.50.12
关键词: Stiffened composite panelsNonlinear buckling analysisFEM ply orientations
全文获取路径: Gruppo Italiano Frattura  (合作)
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关键词翻译
关键词翻译
  • stiffened 加强的
  • buckling 地壳弯曲
  • orientation 定向
  • composite 复合的
  • nonlinear 非线性的
  • panel 
  • analysis 分析
  • FEM Finite-Element Method