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04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage ToleranceSTUDY ON LOW-VELOCITY IMPACT BEHAVIOR AND RESIDUAL PERFORMANCE PREDICTION OF CFRP T-JOINTSJ. Zhou, China; C. Zhang, China Current methods that employ multiple models to assess the mechanical properties of composites exhibit certain limitations. This study develops a combined FE analysis method, based on stress failure criteria and stiffness degradation theory. It transfers element damage states between models, avoiding traditional method inefficiencies and errors in multi-model information transfer. |