Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method
In this study, the stress, strain, and flow blocking effect of the explosion-proof honeycomb structure of a UAV fuel tank are analyzed when it is impacted by continuous fluid caused by explosion, and the main stress concentration areas and overall stress distribution are analyzed. It simplifies the...
| Main Authors: | , , , , , |
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| Format: | Article |
| Language: | English |
| Published: |
Frontiers Media S.A.
2022-08-01
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| Series: | Frontiers in Materials |
| Subjects: | |
| Online Access: | https://www.frontiersin.org/articles/10.3389/fmats.2022.886150/full |
| _version_ | 1811188607855099904 |
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| author | Chunzhi Wang Chunzhi Wang Changbo Lu Xufeng Lin Gaojun An Ximeng Xu Yumeng Gan |
| author_facet | Chunzhi Wang Chunzhi Wang Changbo Lu Xufeng Lin Gaojun An Ximeng Xu Yumeng Gan |
| author_sort | Chunzhi Wang |
| collection | DOAJ |
| description | In this study, the stress, strain, and flow blocking effect of the explosion-proof honeycomb structure of a UAV fuel tank are analyzed when it is impacted by continuous fluid caused by explosion, and the main stress concentration areas and overall stress distribution are analyzed. It simplifies the problem due to the symmetry of the barrier and explosion-proof structure of the UAV fuel tank. Taking a three-layer superposition model of the UAV fuel tank as the research object, the stress and strain of the material structure under detonation impact are analyzed by a bidirectional fluid structure coupling method. The simulation results of choke flow of the fuel tank structure are obtained, which provides reference for the structural optimization design of the honeycomb barrier and explosion-proof material for the UAV. |
| first_indexed | 2024-04-11T14:22:42Z |
| format | Article |
| id | doaj.art-e1d6085591844520871a87bcc0a207f1 |
| institution | Directory Open Access Journal |
| issn | 2296-8016 |
| language | English |
| last_indexed | 2024-04-11T14:22:42Z |
| publishDate | 2022-08-01 |
| publisher | Frontiers Media S.A. |
| record_format | Article |
| series | Frontiers in Materials |
| spelling | doaj.art-e1d6085591844520871a87bcc0a207f12022-12-22T04:19:02ZengFrontiers Media S.A.Frontiers in Materials2296-80162022-08-01910.3389/fmats.2022.886150886150Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling methodChunzhi Wang0Chunzhi Wang1Changbo Lu2Xufeng Lin3Gaojun An4Ximeng Xu5Yumeng Gan6Beijing Institute of New Energy Technology, Beijing, ChinaDepartment of Chemistry, College of Science, China University of Petroleum (East China), Qingdao, ChinaBeijing Institute of New Energy Technology, Beijing, ChinaDepartment of Chemistry, College of Science, China University of Petroleum (East China), Qingdao, ChinaBeijing Institute of New Energy Technology, Beijing, ChinaBeijing Institute of New Energy Technology, Beijing, ChinaBeijing Institute of New Energy Technology, Beijing, ChinaIn this study, the stress, strain, and flow blocking effect of the explosion-proof honeycomb structure of a UAV fuel tank are analyzed when it is impacted by continuous fluid caused by explosion, and the main stress concentration areas and overall stress distribution are analyzed. It simplifies the problem due to the symmetry of the barrier and explosion-proof structure of the UAV fuel tank. Taking a three-layer superposition model of the UAV fuel tank as the research object, the stress and strain of the material structure under detonation impact are analyzed by a bidirectional fluid structure coupling method. The simulation results of choke flow of the fuel tank structure are obtained, which provides reference for the structural optimization design of the honeycomb barrier and explosion-proof material for the UAV.https://www.frontiersin.org/articles/10.3389/fmats.2022.886150/fullUAV fuel tankhoneycomb barrier and explosion-proof structurefluid structure couplingstress-strainchoke flow analysis |
| spellingShingle | Chunzhi Wang Chunzhi Wang Changbo Lu Xufeng Lin Gaojun An Ximeng Xu Yumeng Gan Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method Frontiers in Materials UAV fuel tank honeycomb barrier and explosion-proof structure fluid structure coupling stress-strain choke flow analysis |
| title | Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method |
| title_full | Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method |
| title_fullStr | Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method |
| title_full_unstemmed | Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method |
| title_short | Force analysis of the explosion-proof structure of a UAV fuel tank based on the fluid structure coupling method |
| title_sort | force analysis of the explosion proof structure of a uav fuel tank based on the fluid structure coupling method |
| topic | UAV fuel tank honeycomb barrier and explosion-proof structure fluid structure coupling stress-strain choke flow analysis |
| url | https://www.frontiersin.org/articles/10.3389/fmats.2022.886150/full |
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