Title | Numerical modelling of braided ceramic fiber seals by using element differential method |
Author | |
Corresponding Author | Gao, Xiao-Wei |
Publication Years | 2023-01-15
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DOI | |
Source Title | |
ISSN | 0263-8223
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Volume | 304 |
Abstract | A new kind of dynamic seal with braided ceramic fibers has been designed to seal the movable panels in the scramjet engines, which are used for the propulsion of hypersonic vehicle. The braided ceramic fiber structure can provide buffer forces when the seals are subjected to the external dynamical preloads. However, it also makes the seals difficult to analyze. Up to now, the analysis of the seals still uses 1D models so that one cannot implement the coupled analysis of seals and their surrounding structures and flows. In this paper, a novel 2D and 3D mechanics-thermal-seepage coupled model is proposed to describe these seals, which provides a possibility for the aforementioned coupled analysis. Meanwhile, a strong-form numerical method, element differential method (EDM) is employed to discretize the governing equations of the coupled model due to its efficiency and robustness. Three examples are given. The first one is to invert the material-dependent parameters of three kinds of seal strips from the experimental data by Levenberg-Marquardt (LM) algorithm. Other two implement the analyses of 3D square and circular cross-section seals, respectively, which verify that EDM is more efficient than FEM in seal analysis when using the same mesh sizes. © 2022 Elsevier Ltd |
Indexed By | |
Language | English
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SUSTech Authorship | First
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Funding Project | The support of this investigation by the National Natural Science Foundation of China (Grant Nos. 12072064) is gratefully acknowledged.
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Publisher | |
EI Accession Number | 20224613129294
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EI Keywords | Fibers
; Hypersonic aerodynamics
; Hypersonic vehicles
; Numerical methods
; Ramjet engines
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ESI Classification Code | Pipe Accessories:619.1.1
; Aerodynamics, General:651.1
; Aircraft, General:652.1
; Aircraft Engines, General:653.1
; Spacecraft, General:655.1
; Numerical Methods:921.6
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ESI Research Field | MATERIALS SCIENCE
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Data Source | EV Compendex
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Citation statistics |
Cited Times [WOS]:0
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Document Type | Journal Article |
Identifier | http://kc.sustech.edu.cn/handle/2SGJ60CL/452689 |
Department | Department of Mechanics and Aerospace Engineering |
Affiliation | 1.Department of Mechanics and Aerospace Engineering, Southern University of Science and Technology, Shenzhen; 518055, China 2.School of Aeronautics and Astronautics, Dalian University of Technology, Dalian; 116024, China 3.Key Laboratory of Advanced Technology for Aerospace Vehicles of Liaoning Province, Dalian University of Technology, Dalian; 116024, China 4.State Key Laboratory of Structural Analysis for Industrial Equipment, Dalian University of Technology, Dalian; 116024, China |
First Author Affilication | Department of Mechanics and Aerospace Engineering |
First Author's First Affilication | Department of Mechanics and Aerospace Engineering |
Recommended Citation GB/T 7714 |
Zheng, Yong-Tong,Gao, Xiao-Wei,Liu, Yijun. Numerical modelling of braided ceramic fiber seals by using element differential method[J]. COMPOSITE STRUCTURES,2023,304.
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APA |
Zheng, Yong-Tong,Gao, Xiao-Wei,&Liu, Yijun.(2023).Numerical modelling of braided ceramic fiber seals by using element differential method.COMPOSITE STRUCTURES,304.
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MLA |
Zheng, Yong-Tong,et al."Numerical modelling of braided ceramic fiber seals by using element differential method".COMPOSITE STRUCTURES 304(2023).
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