在飞机结构设计中,为高效完成复合材料加筋板结构设计,亟需一种快速有效的复合材料整体加筋板后屈曲失效评估方法.采用商业有限元软件ABAQUS建立了加筋板有限元模型,研究了复合材料整体加筋板的轴压后屈曲失效评估方法,即“整体局部”法.通过对单筋条壁板后屈曲的失效分析发现,“整体局部”法可得到初始脱胶时的位移和载荷值以及较准确的破坏载荷值,是一种能有效确定加筋板后屈曲失效情况的快速评估方法,对提高结构设计效率和减轻飞机结构质量具有重要的工程意义.
参考文献
| [1] | 朱菊芬,杨海平.复合材料加筋板壳结构的后屈曲强度及破坏分析程序系统[J].计算结构力学及其应用,1996(04):489-493. |
| [2] | 陈桂娟,矫桂琼,熊伟,王忠平.复合材料层合板非线性后屈曲特性的研究[J].武汉科技大学学报（自然科学版）,2005(01):103-107. |
| [3] | Zimmermann R,Rolfes R.POSICOSS improved postbuck ling simulation for design of fibre composite stiffened fuselage structures[J].Composite Structures,2006,73 (2):171-174.,2006. |
| [4] | Degenhardt R,Rolfes R,Zimmermann R,et al.COCOMAT improved material exploitation at safe design of composite airframe structures by accurate simulation of postbuckling and collapse[J].Composite Structures,2006,73(2):175-178.,2006. |
| [5] | Kling A,Degenhardt R,Klein H,et al.Novel stability de sign scenario for aircraft structures simulation and experi mental validation[C]//Proceedings of the 5th International Conference on Computation of Shell and Spatial Structures,2005.,2005. |
| [6] | Zimmermann R,Klein H,Kling A.Buckling and postbuck ling of stringer stiffened fibre composite curved panels-tests and computations[J].Composite Structures,2006,73(2):150-161.,2006. |
| [7] | Degenhardt R,Kling A,Rohwer K,et al.Design and analy sis of stiffened composite panels including post buckling and collapse[J].Computers & Structures,2008,86(9):919-929.,2008. |
| [8] | Koundouros M.In plane compressive behaviour of stiffened thin skinned composite panels with a stress concentrator[D].London:Imperial College London,2005.,2005. |
| [9] | Orifici A C,Shah S A,Herszberg I,et al.Failure analysis in postbuckled composite T sections[J].Composite Struc tures,2008,86(1 3):146-153.,2008. |
| [10] | Orifici A C,Thomson R S,Herszberg I,et al.An analysis methodology for failure in postbucklng skin stiffener inter faces[J].Composite Structures,2008,86(1-3):186-193.,2008. |
| [11] | Orifici A C,de Zarate Alberdi I O,Thomson R S,et al.Compression and post buckling damage growth and collapse analysis of flat composite stiffened panels[J].Composites Science and Technology,2008,68(15 16):3150-3160.,2008. |
| [12] | Orifici A C.Degradation models for the collapse analysis of composite aerospace structures[D].Melbourne:RM1T Uni versity,2007.,2007. |
| [13] | Bertolini J,Castanié B,Barrau J J,et al.An experimental and numerical study on omega stringer debonding[J].Com positeStructures,2008,86(1 3):233-242.,2008. |
| [14] | Bertolini J,Castanié B,Barrau J J,et al.Multi level experi mental and numerical analysis of composite stiffener debond ing.Part 1:Non specific specimen level[J].Composite Structures,2009,90(4):381-391.,2009. |
| [15] | Bertolini J,Castanié B,Barrau J J,et al.Multi level experi mental and numerical analysis of composite stiffener debond ing.Part 2:Element and panel level[J].Composite Struc tures,2009,90(4):392-403.,2009. |
| [16] | 孔斌,叶强报,陈普会,柴亚南.复合材料整体加筋板轴压后屈曲的传载机制[J].复合材料学报,2010(05):142-149. |
| [17] | 孔斌,叶强,陈普会,柴亚南.复合材料整体加筋板轴压后屈曲失效表征[J].复合材料学报,2010(05):150-155. |
| [18] | 孙启星 .复合材料整体加筋壁板的失效分析[D].南京航空航天大学,2008. |
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