A new two-way artificial boundary condition for wave propagation

We propose a new formulation of a two-way artificial boundary condition for the wave equation in mixed form. We justify appropriately the idea behind the formulation of the two-way artificial boundary condition. To exhibit the capabilities of the two-way artificial boundary condition we perform a se...

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Tipo de recurso:
Fecha de publicación:
2017
Institución:
Universidad Tecnológica de Bolívar
Repositorio:
Repositorio Institucional UTB
Idioma:
eng
OAI Identifier:
oai:repositorio.utb.edu.co:20.500.12585/8969
Acceso en línea:
https://hdl.handle.net/20.500.12585/8969
Palabra clave:
Aeroacoustics
Wave propagation
Analytical tests
Artificial boundary condition
Computationally efficient
Finite element codes
Non-linear solver
Two ways
Boundary conditions
Rights
restrictedAccess
License
http://creativecommons.org/licenses/by-nc-nd/4.0/
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network_acronym_str UTB2
network_name_str Repositorio Institucional UTB
repository_id_str
spelling 2020-03-26T16:32:41Z2020-03-26T16:32:41Z201723rd AIAA/CEAS Aeroacoustics Conference, 20179781624105043https://hdl.handle.net/20.500.12585/8969Universidad Tecnológica de BolívarRepositorio UTB56126923400571932065707005744071We propose a new formulation of a two-way artificial boundary condition for the wave equation in mixed form. We justify appropriately the idea behind the formulation of the two-way artificial boundary condition. To exhibit the capabilities of the two-way artificial boundary condition we perform a set of analytical tests. All tests performed are passed satisfactorily which reassures the applicability of the formulation as a two-way artificial boundary condition. The two-way artificial boundary condition does not require non-linear solvers or iterations on the boundary which makes it computationally efficient. Additionally, it can be easily implemented into existing finite element codes. © 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.Recurso electrónicoapplication/pdfengAmerican Institute of Aeronautics and Astronautics Inc, AIAAhttp://creativecommons.org/licenses/by-nc-nd/4.0/info:eu-repo/semantics/restrictedAccessAtribución-NoComercial 4.0 Internacionalhttp://purl.org/coar/access_right/c_16echttps://www.scopus.com/inward/record.uri?eid=2-s2.0-85023637396&partnerID=40&md5=d68613e32db652914cb57d6e3474da5223rd AIAA/CEAS Aeroacoustics Conference, 2017A new two-way artificial boundary condition for wave propagationinfo:eu-repo/semantics/conferenceObjectinfo:eu-repo/semantics/publishedVersionConferenciahttp://purl.org/coar/version/c_970fb48d4fbd8a85http://purl.org/coar/resource_type/c_c94fAeroacousticsWave propagationAnalytical testsArtificial boundary conditionComputationally efficientFinite element codesNon-linear solverTwo waysBoundary conditions5 June 2017 through 9 June 2017Espinoza Román, Héctor GabrielParedes R.J.Ehrhardt M.Tsynkov, S.V., Numerical solution of problems on unbounded domains. A review (1998) Applied Numerical Mathematics, 27 (4), pp. 465-532Espinoza, H., Codina, R., Badia, S., A Sommerfeld non-reecting boundary condition for the wave equation in mixed form (2014) Computer Methods in Applied Mechanics and Engineering, 276 (7), pp. 122-148Fibich, G., Tsynkov, S., High-order two-way artificial boundary conditions for nonlinear wave propagation with backscattering (2001) Journal of Computational Physics, 171 (2), pp. 632-677Fibich, G., Ilan, B., Tsynkov, S., Computation of nonlinear backscattering using a high-order numerical method (2002) Journal of Scientific Computing, 17 (1-4), pp. 351-364Fibich, G., Tsynkov, S., Numerical solution of the nonlinear Helmholtz equation (2008) Effective Computational Methods for Wave Propagation, pp. 37-62. , edited by N. A. Kampanis, V. A. Dougalis, and J. A. Ekatenaris, Chapman and HallCodina, R., Finite element approximation of the hyperbolic wave equation in mixed form (2008) Computer Methods in Applied Mechanics and Engineering, 197 (13-16), pp. 1305-1322Badia, S., Codina, R., Espinoza, H., Stability, Convergence, and Accuracy of Stabilized Finite Element Methods for the Wave Equation in Mixed Form (2014) SIAM Journal on Numerical Analysis, 52 (4-5), pp. 1729-1752Espinoza, H., Codina, R., Badia, S., On some time marching schemes for the stabilized finite element approximation of the mixed wave equation (2015) Computer Methods in Applied Mechanics and Engineering, 296 (11), pp. 295-326Espinoza, H., (2015) Wave Propagation Problems with Aeroacoustic Applications, , Universitat Politécnica de Catalunya, Barcelona, Spainhttp://purl.org/coar/resource_type/c_c94fTHUMBNAILMiniProdInv.pngMiniProdInv.pngimage/png23941https://repositorio.utb.edu.co/bitstream/20.500.12585/8969/1/MiniProdInv.png0cb0f101a8d16897fb46fc914d3d7043MD5120.500.12585/8969oai:repositorio.utb.edu.co:20.500.12585/89692023-05-26 08:37:08.766Repositorio Institucional UTBrepositorioutb@utb.edu.co
dc.title.none.fl_str_mv A new two-way artificial boundary condition for wave propagation
title A new two-way artificial boundary condition for wave propagation
spellingShingle A new two-way artificial boundary condition for wave propagation
Aeroacoustics
Wave propagation
Analytical tests
Artificial boundary condition
Computationally efficient
Finite element codes
Non-linear solver
Two ways
Boundary conditions
title_short A new two-way artificial boundary condition for wave propagation
title_full A new two-way artificial boundary condition for wave propagation
title_fullStr A new two-way artificial boundary condition for wave propagation
title_full_unstemmed A new two-way artificial boundary condition for wave propagation
title_sort A new two-way artificial boundary condition for wave propagation
dc.subject.keywords.none.fl_str_mv Aeroacoustics
Wave propagation
Analytical tests
Artificial boundary condition
Computationally efficient
Finite element codes
Non-linear solver
Two ways
Boundary conditions
topic Aeroacoustics
Wave propagation
Analytical tests
Artificial boundary condition
Computationally efficient
Finite element codes
Non-linear solver
Two ways
Boundary conditions
description We propose a new formulation of a two-way artificial boundary condition for the wave equation in mixed form. We justify appropriately the idea behind the formulation of the two-way artificial boundary condition. To exhibit the capabilities of the two-way artificial boundary condition we perform a set of analytical tests. All tests performed are passed satisfactorily which reassures the applicability of the formulation as a two-way artificial boundary condition. The two-way artificial boundary condition does not require non-linear solvers or iterations on the boundary which makes it computationally efficient. Additionally, it can be easily implemented into existing finite element codes. © 2017, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
publishDate 2017
dc.date.issued.none.fl_str_mv 2017
dc.date.accessioned.none.fl_str_mv 2020-03-26T16:32:41Z
dc.date.available.none.fl_str_mv 2020-03-26T16:32:41Z
dc.type.coarversion.fl_str_mv http://purl.org/coar/version/c_970fb48d4fbd8a85
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dc.type.hasversion.none.fl_str_mv info:eu-repo/semantics/publishedVersion
dc.type.spa.none.fl_str_mv Conferencia
status_str publishedVersion
dc.identifier.citation.none.fl_str_mv 23rd AIAA/CEAS Aeroacoustics Conference, 2017
dc.identifier.isbn.none.fl_str_mv 9781624105043
dc.identifier.uri.none.fl_str_mv https://hdl.handle.net/20.500.12585/8969
dc.identifier.instname.none.fl_str_mv Universidad Tecnológica de Bolívar
dc.identifier.reponame.none.fl_str_mv Repositorio UTB
dc.identifier.orcid.none.fl_str_mv 56126923400
57193206570
7005744071
identifier_str_mv 23rd AIAA/CEAS Aeroacoustics Conference, 2017
9781624105043
Universidad Tecnológica de Bolívar
Repositorio UTB
56126923400
57193206570
7005744071
url https://hdl.handle.net/20.500.12585/8969
dc.language.iso.none.fl_str_mv eng
language eng
dc.relation.conferencedate.none.fl_str_mv 5 June 2017 through 9 June 2017
dc.rights.coar.fl_str_mv http://purl.org/coar/access_right/c_16ec
dc.rights.uri.none.fl_str_mv http://creativecommons.org/licenses/by-nc-nd/4.0/
dc.rights.accessrights.none.fl_str_mv info:eu-repo/semantics/restrictedAccess
dc.rights.cc.none.fl_str_mv Atribución-NoComercial 4.0 Internacional
rights_invalid_str_mv http://creativecommons.org/licenses/by-nc-nd/4.0/
Atribución-NoComercial 4.0 Internacional
http://purl.org/coar/access_right/c_16ec
eu_rights_str_mv restrictedAccess
dc.format.medium.none.fl_str_mv Recurso electrónico
dc.format.mimetype.none.fl_str_mv application/pdf
dc.publisher.none.fl_str_mv American Institute of Aeronautics and Astronautics Inc, AIAA
publisher.none.fl_str_mv American Institute of Aeronautics and Astronautics Inc, AIAA
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institution Universidad Tecnológica de Bolívar
dc.source.event.none.fl_str_mv 23rd AIAA/CEAS Aeroacoustics Conference, 2017
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