A Numerical Method for Strength Analysis of Composite Joints

복합재 체결부 강도해석을 위한 새로운 수치해석방법

  • 강봉수 (경상대학교 대학원 항공공학과) ;
  • 정재우 (경상대학교 대학원 항공공학과) ;
  • 권진회 (경상대학교 기계항공공학부, 항공기부품기술연구센터) ;
  • 최진호 (경상대학교 기계항공공학부, 항공기부품기술연구센터)
  • Published : 2004.04.01

Abstract

A numerical method is presented to determine the characteristic lengths for the failure analysis of composite joints without characteristic length tests. In the conventional methods, compressive characteristic length was determined from the result of a combined bearing test and finite element analysis. The present study, however, shows that the same compressive characteristic length can be obtained by numerical calculation without the bearing test. A new method to define the tensile characteristic length is also introduced so that the tensile characteristic length is numerically determined without the tensile test. Failure loads based on the numerically calculated characteristic lengths are validated by the test results for composite joints

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