Volume 28 Issue 4
Apr.  2002
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JIANG Li, ZHANG Zhi-min. Bucking Delaminating of Composite Sandwich Plates under Hygrothermal Conditions[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(4): 438-442. (in Chinese)
Citation: JIANG Li, ZHANG Zhi-min. Bucking Delaminating of Composite Sandwich Plates under Hygrothermal Conditions[J]. Journal of Beijing University of Aeronautics and Astronautics, 2002, 28(4): 438-442. (in Chinese)

Bucking Delaminating of Composite Sandwich Plates under Hygrothermal Conditions

  • Received Date: 29 Nov 2000
  • Publish Date: 30 Apr 2002
  • To analyze the buckling of elliptical face-core delaminating in composite sandwich plates, a two-dimensional elastic foundation model was established. A displacement function was considered to describe the buckling shapes. By taking the effects of hygrothermal conditions, of the core and of the composite adjacent to delaminating location into account, Reyleigh-Ritz energy method was used to predict the critical buckling load, as a function of composite material, laying angle and hygrothermal condition.

     

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  • [1] Chai H, Babcock C D, Knayss W G. One dimensional modelling of failure laminated plates by delamination buckling[J].Solids and Structure, 1981,17(11):1069~1083. [2]Vizzini A J, Lagace P A. The buckling of a delaminating sublaminate on an elastic foundation[J].Composite Materials, 1987,21(12):1106~1117. [3]张志民.复合材料结构力学[M].北京:北京航空航天大学出版社,1993. [4]徐永锋.含分层损伤复合材料夹层板的压缩剩余强度研究 .北京:北京航空航天大学飞行器设计与应用力学系,1996.
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