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Titlebook: Computational Acoustics; Manfred Kaltenbacher Book 2018 CISM International Centre for Mechanical Sciences 2018 aeroacoustics.computational

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发表于 2025-3-21 19:01:26 | 显示全部楼层 |阅读模式
书目名称Computational Acoustics
编辑Manfred Kaltenbacher
视频video
概述Presents comprehensive physical / mathematical modelling of vibro- and aeroacoustics.Applies state of the art of numerical methods (Finite Elements, Boundary Elements, Discontinuous Galerkin).Comprehe
丛书名称CISM International Centre for Mechanical Sciences
图书封面Titlebook: Computational Acoustics;  Manfred Kaltenbacher Book 2018 CISM International Centre for Mechanical Sciences 2018 aeroacoustics.computational
描述.The book presents a state-of-art overview of numerical schemes efficiently solving the acoustic conservation equations (unknowns are acoustic pressure and particle velocity) and the acoustic wave equation (pressure of acoustic potential formulation). Thereby, the different equations model both vibrational- and flow-induced sound generation and its propagation. Latest numerical schemes as higher order finite elements, non-conforming grid techniques, discontinuous Galerkin approaches and boundary element methods are discussed. Main applications will be towards aerospace, rail and automotive industry as well as medical engineering. The team of authors are able to address these topics from the engineering as well as numerical points of view..
出版日期Book 2018
关键词aeroacoustics; computational aeroacoustics; numerical simulation; acoustic wave equation; finite element
版次1
doihttps://doi.org/10.1007/978-3-319-59038-7
isbn_softcover978-3-319-86537-9
isbn_ebook978-3-319-59038-7Series ISSN 0254-1971 Series E-ISSN 2309-3706
issn_series 0254-1971
copyrightCISM International Centre for Mechanical Sciences 2018
The information of publication is updating

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发表于 2025-3-21 21:14:17 | 显示全部楼层
Marko M. Popovic,Svetozar S. Popoviclexibility to choose for each sub-domain an optimal grid. The two proposed methods - Mortar and Nitsche-type mortaring - fulfill the physical conditions along the non-conforming interfaces. We exploit this capability and apply it to real engineering applications in aeroacoustics. The results clearly
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Marko M. Popovic,Svetozar S. Popovictz equation with admittance boundary conditions is solved in 3d. The chapter starts with a derivation of the Kirchhoff–Helmholtz integral equation from a residual formulation of the Helmholtz equation. The discretization process with introduction of basis and test functions is described and shown fo
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Computational Acoustics978-3-319-59038-7Series ISSN 0254-1971 Series E-ISSN 2309-3706
发表于 2025-3-23 03:26:42 | 显示全部楼层
https://doi.org/10.1007/978-3-319-59038-7aeroacoustics; computational aeroacoustics; numerical simulation; acoustic wave equation; finite element
发表于 2025-3-23 06:35:45 | 显示全部楼层
978-3-319-86537-9CISM International Centre for Mechanical Sciences 2018
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