Thermo-mechanical characteristics of pre-tensioned fiber fabrics subjected to hypervelocity impact

XU Huadong; YU Dong; WANG Yulin; SHI Jingfu; LIU Lei; SONG Di; MIAO Changqing

doi:10.11883/bzycj-2021-0307

Volume 42 Issue 5

May 2022

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XU Huadong, YU Dong, WANG Yulin, SHI Jingfu, LIU Lei, SONG Di, MIAO Changqing. Thermo-mechanical characteristics of pre-tensioned fiber fabrics subjected to hypervelocity impact[J]. Explosion And Shock Waves, 2022, 42(5): 053301. doi: 10.11883/bzycj-2021-0307

Citation:

XU Huadong, YU Dong, WANG Yulin, SHI Jingfu, LIU Lei, SONG Di, MIAO Changqing. Thermo-mechanical characteristics of pre-tensioned fiber fabrics subjected to hypervelocity impact[J]. Explosion And Shock Waves, 2022, 42(5): 053301. doi: 10.11883/bzycj-2021-0307

Citation:

XU Huadong, YU Dong, WANG Yulin, SHI Jingfu, LIU Lei, SONG Di, MIAO Changqing. Thermo-mechanical characteristics of pre-tensioned fiber fabrics subjected to hypervelocity impact[J]. Explosion And Shock Waves, 2022, 42(5): 053301. doi: 10.11883/bzycj-2021-0307

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Thermo-mechanical characteristics of pre-tensioned fiber fabrics subjected to hypervelocity impact

doi: 10.11883/bzycj-2021-0307

1.
National Key Laboratory of Science and Technology on Advanced Composites in Special Environments, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China
2.
Department of Mechanical Design, School of Mechatronics Engineering, Harbin Institute of Technology, Harbin 150001, Heilongjiang, China
3.
China Academy of Launch Vehicle Technology, Beijing 100076, China
4.
School of Mechanical and Electrical Engineering, University of Electronic Science and Technology of China, Chengdu 611731, Sichuan, China

Received Date: 2021-07-20
Rev Recd Date: 2021-11-01

Available Online: 2022-04-06

Publish Date: 2022-05-27

Abstract

Abstract

In an inflatable capsule, a bearing layer, which consists of high-performance fiber fabrics, is always used to bear its internal pressure load and to provide space debris protection. The pre-tension of the fiber fabric bearing layer, resulting from the pressure load, has a significant effect on the characteristics of the fiber fabric under space debris hypervelocity impact, thereby affecting the space debris protection performance of the inflatable capsule. To consider the thermo-mechanical behavior during hypervelocity impact, a numerical model for hypervelocity impact on pre-tensioned fiber fabrics is developed by introducing the Johnson-Cook strength model and Mie-Grüneisen state equation. The finite element method-smoothed particle hydrodynamics (FEM-SPH) coupling algorithm is used to discrete the yarn weaving structure of fiber fabrics. A fabric panel that has a rectangular configuration is pre-stretched by applying tensile stress boundary conditions. A projectile is then launched at a preset velocity and hit the four-side clamped pre-tensioned fiber fabric to simulate the hypervelocity impact process. The thermal-mechanical properties and space debris protection performance of the pre-tensioned fiber fabrics under hypervelocity impact are analyzed. The results show that with an increase in pre-tension, the perforation diameter of the fiber fabric increases, while the diffusion angle of the debris, as well as the absorption rate of the projectile kinetic energy and the temperature of the impact area, decrease. As a result, the pre-tension significantly reduces the space debris protection performance of the fiber fabrics.
- hypervelocity impact,
- fiber fabric,
- thermo-mechanical properties,
- inflatable capsule,
- space debris

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References(29)

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