MIXED-MODE BENDING METHOD FOR DELAMINATION TESTING

被引:427
作者
REEDER, JR
CREWS, JH
机构
[1] NASA Langley Research Center, Materials Division, Mechanics of Materials Branch, Hampton, VA
关键词
D O I
10.2514/3.25204
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A mixed-mode delamination test procedure was developed combining double cantilever beam (DCB) mode I loading and end-notch flexure (ENF) mode II loading on a split unidirectional laminate. By loading with a lever, a single applied load simultaneously produces mode I and mode II bending loads on the specimen. This mixed-mode bending (MMB) test was analyzed using both finite-element procedures and beam theory to calculate the mode I and mode II components of strain-energy release rate GI and GII, respectively. A wide range of GI/GII ratios can be produced by varying the load position on the lever. As the delamination extended, the GI/GII ratios varied by less than 5%. Beam theory equations agreed closely with the finite-element results and provide a basis for selection of GI/GII test ratios and a basis for computing the mode I and mode II components of measured delamination toughness. The MMB test was demonstrated using AS4/PEEK (APC2) unidirectional laminates. The MMB test introduced in this paper is rather simple and is believed to offer several advantages over most current mixed-mode test. © 1990 American Institute of Aeronautics and Astronautics, Inc., All rights reserved.
引用
收藏
页码:1270 / 1276
页数:7
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