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A Ply-By-Ply Discretized 2D FEA Approach with the Integrated XFEM-CE Strategy for Predicting Multiple Failures in Laminated Composite Structures

Yana Wang1,2,3,4, Ruodi Jia1,5, Fengrui Liu1,5,6,*

School of Astronautics, Beihang University, Beijing, 100191, China.
Aeronautical Material Testing Research Center, AECC Beijing Institute of Aeronautical Materials, Beijing, 100095, China.
Beijing Key Laboratory of Aeronautical Material Testing and Evaluation, Beijing, 100095, China.
Key Laboratory of Aeronautical Material Testing and Evaluation, Aero Engine Corporation of China, Beijing, 100095, China.
Key Laboratory of Spacecraft Design Optimization and Dynamic Simulation Technologies, Minisitry of Education, Beihang University, Beijing, 100191, China.
State Key Laboratory for Strength and Vibration of Mechanical Structures, Xi’an Jiaotong University, Xi’an, 710049, China.

*Corresponding Author: Fengrui Liu. Email: email.

TSP_CMES_6542.pdf

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