Journal of Astronautics ›› 2021, Vol. 42 ›› Issue (11): 1475-1482.doi: 10.3873/j.issn.1000-1328.2021.11.014

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Modeling and Analysis of Thermo Mechanical Behavior for Fiber Fabric under Hypervelocity Impact

ZHANG Yi,WANG Yu lin,SHI Jing fu,YU Dong,XU Hua dong,MA Fu jian,SONG Di,MIAO Chang qing   

  1. 1.National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150001, China; 2. Department of Aerospace Research and Exploration, China Academy of Launch Vehicle Technology, Beijing 100076, China; 3. Department of Mechanical Design, School of Mechanical and Electrical Engineering, Harbin Institute of Technology, Harbin 150001, China; 4. China Aerodynamics Research and Development Center, Mianyang 621000, China;5.School of Mechanical and Electrical Engineering,University of Electronic Science and Technology of China, Chengdu, 611731, China

  • Received:2021-01-14 Revised:2021-03-31 Online:2021-11-15 Published:2021-11-15

Abstract: A new thermo mechanical model for fiber fabric of hypervelocity impact is established by using the Johnson Cook model, the Gruneisen equation of state and the FEM SPH coupling algorithm, while some new factors are taken into account such as the heat generation, strain rate strengthening and high temperature softening of materials. Mechanical and thermal information could be obtained with the model, such as penetration, fragmentation, stress and strain, heat generation and temperature field of fiber fabric. The analysis results are in good agreement with the experimental results.

Key words: Fiber fabric, Hypervelocity impact, Johnson Cook model, Orbital debris shielding, Unit cell model

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