期刊文献+

双轴应力下含裂纹加筋曲板剩余强度的弹塑性有限元计算

AN ELASTIC PLASTIC FINITE ELEMENT ANALYSIS OF CRACKED STIFFENED CURVED PANEL UNDER BIAXIAL STRESS
下载PDF
导出
摘要 采用考虑了大应变的弹塑性有限元方法,以裂纹尖端张开角为断裂准则,实现了双向受载条件下加筋曲板中裂纹起裂到失稳整个扩展过程的数值模拟计算;还对与加筋曲板有同样尺寸的加筋平板进行了分析和计算。结果表明,所提出的分析方法和所采用的断裂准则适用于对含裂纹加筋结构所进行的剩余强度分析。 An elastic plastic finite element method based on incremental theory of plasticity accounting for large strain is made for the prediction of the residual strength of crack stiffened curved panels under biaxial loading. Using the crack tip opening angle (CTOA) as the fracture criterion controlling stable crack extension, the entire process from the initiation of crack growth up to the instability of crack extention is simulated, the residual strength and crack tolerance are presented and some complex mechanics phenomena are found.The results show that the analytic method presented and the fracture criterion adopted are suitable for the residual strength prediction of cracked stiffened structure, the increasing curvature of the cracked stiffened curved panel can change remarkably the stress, strain and displacement field around crack tip and will reduce considerably the loading capability of the cracked stiffened structure.
机构地区 西北工业大学
出处 《航空学报》 EI CAS CSCD 北大核心 1991年第2期B087-B093,共7页 Acta Aeronautica et Astronautica Sinica
关键词 剩余强度 弹塑性 有限元 飞机 曲板 residual strength, elastic plastic finite element method, curved stiffened panel, fracture criterion.
  • 相关文献

参考文献3

  • 1官中信,Eng Fract Mech,1988年,30卷,4期,415页
  • 2陆富梅,1987年
  • 3安俊平,1986年

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