LOCAL CRIPPLING OF THIN-WALLED GRAPHITE-EPOXY STIFFENERS

被引:9
作者
BONANNI, DL
JOHNSON, ER
STARNES, JH
机构
[1] VIRGINIA POLYTECH INST & STATE UNIV,DEPT AEROSP & OCEAN ENGN,BLACKSBURG,VA 24061
[2] NASA,LANGLEY RES CTR,DIV STRUCT MECH,AIRCRAFT STRUCT BRANCH,HAMPTON,VA 23665
关键词
D O I
10.2514/3.10824
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Results from an experimental and analytical study of the local buckling, postbuckling, and crippling (failure) behavior of channel, zee, and I- and J-section stiffeners made of AS4/3502 graphite-epoxy unidirectional tape are presented. Thirty-six specimens were tested in axial compression. Experimental results indicate the existence of a number of damage-initiation modes, all of which involve either delamination in some part of the specimen or local material strength failure in a corner of the specimen. The flange width-to-thickness ratio is found to influence the mode of damage initiation. The inner corner radius strongly affects the crippling stress for the I- and J-section specimens, but was not found to have a significant effect on the crippling stress of channels and zees. Geometrically nonlinear analyses of five specimens were performed with the STAGS general-purpose computer code. Correlation between analytical and experimental results is excellent through buckling, but agreement degrades in postbuckling. The discrepancies in postbuckling are attributed to the neglect of transverse shearing deformations in the analysis and development of damage in the specimens. The maximum compressive fiber stress-failure criterion correlates reasonably well with the first major damage event observed in the tests.
引用
收藏
页码:1951 / 1959
页数:9
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