복합적층판 기계적 체결부에 대한 층간응력해석
This method surely needs a hole that causes local strength and stiffness deterioration of the structure because of stress intensity. In this work, three dimensional stress analysis of pin-loaded joint for quasi-isotropic composite laminates was performed using commercial finite element software. Str...
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Published in | 大韓造船學會 論文集 Vol. 40; no. 6; pp. 49 - 57 |
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Main Authors | , |
Format | Journal Article |
Language | Korean |
Published |
대한조선학회
2003
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Subjects | |
Online Access | Get full text |
ISSN | 1225-1143 2287-7355 |
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Summary: | This method surely needs a hole that causes local strength and stiffness deterioration of the structure because of stress intensity. In this work, three dimensional stress analysis of pin-loaded joint for quasi-isotropic composite laminates was performed using commercial finite element software. Stress distribution was calculated near the edge of the pin-leaded hole and effects of the stacking sequence on the delamination were investigated. Also, the delamination strength of the composite laminates was predicted using the Ye-delamination failure criterion and compared with the experimental results. finally, newly modified failure criterion has been suggested owing to the consideration of effects of interlaminar normal stress on the delamination strength. |
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Bibliography: | KISTI1.1003/JNL.JAKO200311922056624 |
ISSN: | 1225-1143 2287-7355 |