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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Bibliographic Details
Published in大韓造船學會 論文集 Vol. 40; no. 6; pp. 49 - 57
Main Authors 안용택(Y. T. An), 송관형(K. H. Song)
Format Journal Article
LanguageKorean
Published 대한조선학회 2003
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ISSN1225-1143
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.
Bibliography:KISTI1.1003/JNL.JAKO200311922056624
ISSN:1225-1143
2287-7355