Xu Cao , Jianqiu Zhou , Huadong Xu , Di Song , Changqing Miao
{"title":"基于碎片映射法的多板结构超高速碰撞仿真SPH模型重构框架","authors":"Xu Cao , Jianqiu Zhou , Huadong Xu , Di Song , Changqing Miao","doi":"10.1016/j.asr.2025.03.047","DOIUrl":null,"url":null,"abstract":"<div><div>Smoothed Particle Hydrodynamics (SPH) method is widely used in hypervelocity impact analysis, but it is computationally inefficient for common multiplate structures, such as multi-shock, mesh double-bumper, and stuffed shields. To improve the efficiency and accuracy of the SPH method, a reconstruction framework is proposed, including a fragment identification method, a fragment mapping method, and a sequential modeling and simulation approach. In the reconstruction framework, the total impact simulation of a multiplate structure consisting of <em>n</em> plates is decomposed into <em>n</em> individual impacts on each plate. To reduce the computation for each impact, a fragment identification method and a fragment mapping method are developed. Fragments generated from the impact with the <em>i</em>-th plate (<em>i</em> < <em>n</em>) are identified and mapped to the near positions in front of the (<em>i</em> + 1)-th plate using a linear motion algorithm. To reduce the total computation time, a sequential modeling and simulation approach is introduced, only the fragments from the <em>i</em>-th impact and the SPH model of the (<em>i</em> + 1)-th plate of the multiplate structure are reconstructed and simulated sequentially, excluding the other plates. The results show a significant improvement in computational efficiency compared to the traditional SPH method. For a three-layer structure with a 100 mm spacing, the efficiency is 59.2 times larger, while for a double-layer structure with a 350 mm spacing, the efficiency is 201.74 times larger. Moreover, the interactions between fragments are considered in the reconstruction framework, thereby the accuracy of the simulation is also improved.</div></div>","PeriodicalId":50850,"journal":{"name":"Advances in Space Research","volume":"75 11","pages":"Pages 8140-8157"},"PeriodicalIF":2.8000,"publicationDate":"2025-03-26","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"An SPH model reconstruction framework with fragment mapping method for multiplate structure hypervelocity impact simulation\",\"authors\":\"Xu Cao , Jianqiu Zhou , Huadong Xu , Di Song , Changqing Miao\",\"doi\":\"10.1016/j.asr.2025.03.047\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Smoothed Particle Hydrodynamics (SPH) method is widely used in hypervelocity impact analysis, but it is computationally inefficient for common multiplate structures, such as multi-shock, mesh double-bumper, and stuffed shields. To improve the efficiency and accuracy of the SPH method, a reconstruction framework is proposed, including a fragment identification method, a fragment mapping method, and a sequential modeling and simulation approach. In the reconstruction framework, the total impact simulation of a multiplate structure consisting of <em>n</em> plates is decomposed into <em>n</em> individual impacts on each plate. To reduce the computation for each impact, a fragment identification method and a fragment mapping method are developed. Fragments generated from the impact with the <em>i</em>-th plate (<em>i</em> < <em>n</em>) are identified and mapped to the near positions in front of the (<em>i</em> + 1)-th plate using a linear motion algorithm. To reduce the total computation time, a sequential modeling and simulation approach is introduced, only the fragments from the <em>i</em>-th impact and the SPH model of the (<em>i</em> + 1)-th plate of the multiplate structure are reconstructed and simulated sequentially, excluding the other plates. The results show a significant improvement in computational efficiency compared to the traditional SPH method. For a three-layer structure with a 100 mm spacing, the efficiency is 59.2 times larger, while for a double-layer structure with a 350 mm spacing, the efficiency is 201.74 times larger. Moreover, the interactions between fragments are considered in the reconstruction framework, thereby the accuracy of the simulation is also improved.</div></div>\",\"PeriodicalId\":50850,\"journal\":{\"name\":\"Advances in Space Research\",\"volume\":\"75 11\",\"pages\":\"Pages 8140-8157\"},\"PeriodicalIF\":2.8000,\"publicationDate\":\"2025-03-26\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Advances in Space Research\",\"FirstCategoryId\":\"89\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0273117725002868\",\"RegionNum\":3,\"RegionCategory\":\"地球科学\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ASTRONOMY & ASTROPHYSICS\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Advances in Space Research","FirstCategoryId":"89","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0273117725002868","RegionNum":3,"RegionCategory":"地球科学","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ASTRONOMY & ASTROPHYSICS","Score":null,"Total":0}
An SPH model reconstruction framework with fragment mapping method for multiplate structure hypervelocity impact simulation
Smoothed Particle Hydrodynamics (SPH) method is widely used in hypervelocity impact analysis, but it is computationally inefficient for common multiplate structures, such as multi-shock, mesh double-bumper, and stuffed shields. To improve the efficiency and accuracy of the SPH method, a reconstruction framework is proposed, including a fragment identification method, a fragment mapping method, and a sequential modeling and simulation approach. In the reconstruction framework, the total impact simulation of a multiplate structure consisting of n plates is decomposed into n individual impacts on each plate. To reduce the computation for each impact, a fragment identification method and a fragment mapping method are developed. Fragments generated from the impact with the i-th plate (i < n) are identified and mapped to the near positions in front of the (i + 1)-th plate using a linear motion algorithm. To reduce the total computation time, a sequential modeling and simulation approach is introduced, only the fragments from the i-th impact and the SPH model of the (i + 1)-th plate of the multiplate structure are reconstructed and simulated sequentially, excluding the other plates. The results show a significant improvement in computational efficiency compared to the traditional SPH method. For a three-layer structure with a 100 mm spacing, the efficiency is 59.2 times larger, while for a double-layer structure with a 350 mm spacing, the efficiency is 201.74 times larger. Moreover, the interactions between fragments are considered in the reconstruction framework, thereby the accuracy of the simulation is also improved.
期刊介绍:
The COSPAR publication Advances in Space Research (ASR) is an open journal covering all areas of space research including: space studies of the Earth''s surface, meteorology, climate, the Earth-Moon system, planets and small bodies of the solar system, upper atmospheres, ionospheres and magnetospheres of the Earth and planets including reference atmospheres, space plasmas in the solar system, astrophysics from space, materials sciences in space, fundamental physics in space, space debris, space weather, Earth observations of space phenomena, etc.
NB: Please note that manuscripts related to life sciences as related to space are no more accepted for submission to Advances in Space Research. Such manuscripts should now be submitted to the new COSPAR Journal Life Sciences in Space Research (LSSR).
All submissions are reviewed by two scientists in the field. COSPAR is an interdisciplinary scientific organization concerned with the progress of space research on an international scale. Operating under the rules of ICSU, COSPAR ignores political considerations and considers all questions solely from the scientific viewpoint.