Fiber Reinforced Plastics/Composites ›› 2019, Vol. 0 ›› Issue (7): 34-38.

• BASIC STUDY • Previous Articles     Next Articles

NUMERICAL STUDY AND EXPERIMENT OF COMPOSITE STRINGER ON COMPRESSIVE PROPERTY

YE Ti, YUE Yuan   

  1. Aviation Engineering Institute, Civil Aviation Flight University of China, Guanghan 618307, China
  • Received:2018-10-11 Online:2019-07-28 Published:2019-07-28

Abstract: Based on the progressive damage analysis, compressive property of composite stringer was studied with the 3D HASHIN criterion and nonlinear stiffness degradation method. By coding the user-defined material subroutine (UMAT), the application of failure criterion and stiffness degradation method were implemented in ABAQUS. With different sizes and lay-ups into consideration, three dimensional finite element models were built to analyze the compressive property and the failure process, and experimental verification was made simultaneously. For configuration 1,the result of finite element analysis was 247 kN, which agreed well with the experimental result 257 kN, verifying the reliability of the model.

Key words: numerical study, experiment, progressive damage, compressive property, stringer

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