COMPOSITES SCIENCE AND ENGINEERING ›› 2026, Vol. 0 ›› Issue (8): 115-123.DOI: 10.19936/j.cnki.2096-8000.20260828.015

• DESIGN AND TECHNIQUE • Previous Articles     Next Articles

Study on the effect of repair techniques on the residual strength of asymmetric composites

MA Mingze1, MENG Qingchun2, XIONG Xin2, WANG Shiming1, WU Fuqiang3*, WANG Guanhua1   

  1. 1. College of General Aviation and Flight, Nanjing University of Aeronautics and Astronautics,Changzhou 213300, China;
    2. AVIC China Helicopter Research and Development Institute, Jingdezhen 333000, China;
    3. Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
  • Received:2025-06-05 Online:2026-08-28 Published:2026-09-24

Abstract: A study was conducted on the residual strength of asymmetrical composite materials after scratch damage repair. Tensile tests were performed on composite specimens repaired using both patch and scarf repair techniques to compare the effectiveness of different repair methods. A numerical simulation model was developed to analyze the repaired specimens, and the accuracy of the model was validated by comparing the simulation results with experimental data. To further investigate the influence of repair parameters on the effectiveness of scarf repairs, the ultimate loads for different overlap widths were calculated, and the optimal strength recovery factors corresponding to various thicknesses and overlap configurations were determined. The results show that the patch repair technique is effective for surface scratch damage, achieving up to 90% strength recovery. The stepped scarf repair method demonstrated better performance than the double-layer lap repair. However, the repair effectiveness decreases with increasing composite thickness.

Key words: asymmetrical composite materials, scratch damage, repair techniques, strength recovery factor

CLC Number: