Ballistic impact behavior of thin nickel-base alloy plates at different temperatures
To study the aeroengine containment capability in high temperature, experiments and numerical simulations of the spherical nosed projectile impacting thin plate under 25 ℃ and 600 ℃ were performed. Experiments were conducted by using a gas gun. Target plates were impacted by bullets with different i...
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Format: | Article |
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Journal of Aeronautical Materials
2019-01-01
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Series: | Journal of Aeronautical Materials |
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Online Access: | http://jam.biam.ac.cn/CN/Y2019/V39/I1/79 |
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author | LIU Jiao ZHENG Bailin YANG Biao YU Xiaoqiang ZHANG Kai SHI Tongcheng |
author_facet | LIU Jiao ZHENG Bailin YANG Biao YU Xiaoqiang ZHANG Kai SHI Tongcheng |
author_sort | LIU Jiao |
collection | DOAJ |
description | To study the aeroengine containment capability in high temperature, experiments and numerical simulations of the spherical nosed projectile impacting thin plate under 25 ℃ and 600 ℃ were performed. Experiments were conducted by using a gas gun. Target plates were impacted by bullets with different initial velocities. The effect of temperature and initial velocity on the deformation, failure pattern and energy absorption of the plate were analyzed. The results show that at higher temperature, the deformation of the target plates is greater, the energy absorbed by the target plates is smaller and the critical ballistic velocities are smaller . The petal deformation of the target plate caused by bending is more obvious under 600 ℃. Numerical simulations of the impact were conducted by using an explicit dynamics FE code (LS-DYNA). The Johnson-Cook material model was used to carry out the analysis. The Johnson-Cook material model parameters were obtained by the separated Hopkinson pressure bar (SHPB) experiment at high temperature. The results obtained from the numerical simulations were compared with those from the experiments. Good correlation is found between experiments and numerical simulations. |
first_indexed | 2024-04-14T02:21:15Z |
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id | doaj.art-ad2ff1f88d3b4ab9b35131cf9384ef3b |
institution | Directory Open Access Journal |
issn | 1005-5053 1005-5053 |
language | zho |
last_indexed | 2024-04-14T02:21:15Z |
publishDate | 2019-01-01 |
publisher | Journal of Aeronautical Materials |
record_format | Article |
series | Journal of Aeronautical Materials |
spelling | doaj.art-ad2ff1f88d3b4ab9b35131cf9384ef3b2022-12-22T02:18:02ZzhoJournal of Aeronautical MaterialsJournal of Aeronautical Materials1005-50531005-50532019-01-01391798810.11868/j.issn.1005-5053.2018.000045201901000045Ballistic impact behavior of thin nickel-base alloy plates at different temperaturesLIU Jiao0ZHENG Bailin1YANG Biao2YU Xiaoqiang3ZHANG Kai4SHI Tongcheng5School of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092,ChinaSchool of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092,ChinaSchool of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092,ChinaSchool of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092,ChinaSchool of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 200092,ChinaAECC Commercial Aircraft Engine Co., Ltd, Design Research Center, Shanghai 201100,ChinaTo study the aeroengine containment capability in high temperature, experiments and numerical simulations of the spherical nosed projectile impacting thin plate under 25 ℃ and 600 ℃ were performed. Experiments were conducted by using a gas gun. Target plates were impacted by bullets with different initial velocities. The effect of temperature and initial velocity on the deformation, failure pattern and energy absorption of the plate were analyzed. The results show that at higher temperature, the deformation of the target plates is greater, the energy absorbed by the target plates is smaller and the critical ballistic velocities are smaller . The petal deformation of the target plate caused by bending is more obvious under 600 ℃. Numerical simulations of the impact were conducted by using an explicit dynamics FE code (LS-DYNA). The Johnson-Cook material model was used to carry out the analysis. The Johnson-Cook material model parameters were obtained by the separated Hopkinson pressure bar (SHPB) experiment at high temperature. The results obtained from the numerical simulations were compared with those from the experiments. Good correlation is found between experiments and numerical simulations.http://jam.biam.ac.cn/CN/Y2019/V39/I1/79ballistic impact experimentsnumerical simulationtemperaturesJohnson-Cook modelfailure patternscritical ballistic velocity |
spellingShingle | LIU Jiao ZHENG Bailin YANG Biao YU Xiaoqiang ZHANG Kai SHI Tongcheng Ballistic impact behavior of thin nickel-base alloy plates at different temperatures Journal of Aeronautical Materials ballistic impact experiments numerical simulation temperatures Johnson-Cook model failure patterns critical ballistic velocity |
title | Ballistic impact behavior of thin nickel-base alloy plates at different temperatures |
title_full | Ballistic impact behavior of thin nickel-base alloy plates at different temperatures |
title_fullStr | Ballistic impact behavior of thin nickel-base alloy plates at different temperatures |
title_full_unstemmed | Ballistic impact behavior of thin nickel-base alloy plates at different temperatures |
title_short | Ballistic impact behavior of thin nickel-base alloy plates at different temperatures |
title_sort | ballistic impact behavior of thin nickel base alloy plates at different temperatures |
topic | ballistic impact experiments numerical simulation temperatures Johnson-Cook model failure patterns critical ballistic velocity |
url | http://jam.biam.ac.cn/CN/Y2019/V39/I1/79 |
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