期刊文献+

复合材料端框渐进损伤分析方法与试验 被引量:4

Progressive damage analysis method and experimental investigation of composite end frame structure
下载PDF
导出
摘要 针对复合材料格栅加筋圆筒的上下端框,进行了3种不同尺寸和铺层顺序的端框片段模型的拉伸试验,得出其破坏形式和极限载荷.建立端框的有限元模型,基于不同的强度理论进行端框的渐进损伤分析,并对计算结果进行比较.以Zinoviev强度理论为基础,从破坏判据和刚度衰减两方面将其扩展为三维理论,并结合Hashin准则进行破坏模式的判断,形成了改进的Zinoviev强度理论,并以此进行端框模型的损伤演化分析和强度预报,数值模拟结果与试验结果取得了很好的一致性. Aiming at the upper and lower end frames of the grid stiffened composite cylinder,the tensile tests of three kinds of end frame segment models with different sizes and stacking sequence were conducted.Thus the damage forms and ultimate load of the end frames were gained.The progressive damage analysis based on various strength theories was conducted by finite element method,and the results of different theories were compared.Based on Zinoviev strength theory,by expanding its failure criterion and stiffness degradation scheme to three-dimensional format,and introducing Hashin criterion to estimate the damage modes,the modified Zinoviev theory was developed.The proposed method was used to carry out damage evolution analysis and strength prediction of the end frame model.The results of numerical simulation show good agreement with test results.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2012年第7期931-935,共5页 Journal of Beijing University of Aeronautics and Astronautics
基金 国家973计划资助项目(2011CB606105)
关键词 复合材料端框 渐进损伤分析 改进的Zinoviev理论 损伤演化 composite end frame progressive damage analysis modified Zinoviev theory damage evolution
  • 相关文献

参考文献12

  • 1杜善义.先进复合材料与航空航天[J].复合材料学报,2007,24(1):1-12. 被引量:1006
  • 2燕瑛,刘玉佳,廖宝华,闫伟.先进复合材料格栅结构与大型飞机[J].航空制造技术,2009,52(2):26-29. 被引量:6
  • 3杜善义,章继峰,张博明.先进复合材料格栅结构(AGS)应用与研究进展[J].航空学报,2007,28(2):419-424. 被引量:42
  • 4Labossiere P,Neal K W. Macroscopic failure criteria for fiber-re- inforced composite materials [ J]. Solid Mech Arch, 1987, 12 (2) :65 -95. 被引量:1
  • 5Hashin Z. Failure criteria for unidirectional fiber composites [ J ]. Journal of Applied Mechanics, 1980,47 ( 2 ) :329 - 334. 被引量:1
  • 6Puck A, Schurmann H. Failure analysis of FRP laminates by means of physically based phenomenological models [ J ]. Comp Sci & Tech,2002,62(12/13) :1633 -1662. 被引量:1
  • 7Liu K S,Tsai S W. A progressive quadratic failure criterion of a laminate [ J ]. Comp Sci & Tech, 1998,55 (7) : 1023 - 1032. 被引量:1
  • 8Schuhe K. World wide failure exercise on failure prediction in composites[ J]. Comp Sci & Tech,2002,62 ( 12/13 ) :1479. 被引量:1
  • 9Czichon S, Zimmermann K, Middendorf P, et al. Three-dimen- sional stress and progressive failure analysis of ultra thick lami- nates and experimental validation [ J]. Composite Structures, 2011,93 ( 5 ) : 1394 - 1403. 被引量:1
  • 10MSC. Marc 2010 Volume A:theory and user information[ R]. MSC Software ,2010. 被引量:1

二级参考文献88

共引文献1079

同被引文献41

引证文献4

二级引证文献14

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部