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Cited 3 time in webofscience Cited 2 time in scopus
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Coarray Fortran Parallel Implementation of a Finite Volume Method-Based Aircraft Ice Accretion Simulation Code

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dc.contributor.authorRaj, L. Prince-
dc.contributor.authorEsmaeilifar, E.-
dc.contributor.authorSengupta, B.-
dc.contributor.authorJeong, H.-
dc.contributor.authorMyong, R. S.-
dc.date.accessioned2023-06-09T08:40:20Z-
dc.date.available2023-06-09T08:40:20Z-
dc.date.issued2023-09-
dc.identifier.issn2093-274X-
dc.identifier.issn2093-2480-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/59624-
dc.description.abstractThe aircraft industry often uses computational methods to quantify ice accretion, investigate aerodynamic penalties, and conduct certification processes. The computational simulation of aircraft icing is computationally intensive owing to three consecutive runs of air, droplet, and ice accretion solvers. This study developed a parallel code using MPI and Coarray methods to reduce the computation time of an FVM-based ice accretion solver. The computational results were validated by comparison with the experimental data. The parallel performance of the MPI and Coarray methods were compared and found to be similar on the airflow solver. Further, the Coarray-based implementation on the water droplet solver showed good speedup and efficiency for the given number of mesh elements and processors.-
dc.format.extent12-
dc.language영어-
dc.language.isoENG-
dc.publisherThe Korean Society for Aeronautical & Space Sciences-
dc.titleCoarray Fortran Parallel Implementation of a Finite Volume Method-Based Aircraft Ice Accretion Simulation Code-
dc.title.alternativeCoarray Fortran Parallel Implementation of a Finite Volume Method-Based Aircraft Ice Accretion Simulation Code-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.doi10.1007/s42405-023-00601-8-
dc.identifier.scopusid2-s2.0-85160354274-
dc.identifier.wosid000995297900001-
dc.identifier.bibliographicCitationInternational Journal of Aeronautical and Space Sciences, v.24, no.4, pp 1124 - 1135-
dc.citation.titleInternational Journal of Aeronautical and Space Sciences-
dc.citation.volume24-
dc.citation.number4-
dc.citation.startPage1124-
dc.citation.endPage1135-
dc.type.docTypeArticle-
dc.identifier.kciidART003003865-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassscie-
dc.description.journalRegisteredClassscopus-
dc.description.journalRegisteredClasskci-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalWebOfScienceCategoryEngineering, Aerospace-
dc.subject.keywordPlusSCHEME-
dc.subject.keywordAuthorCFD-
dc.subject.keywordAuthorMulti-phase flow-
dc.subject.keywordAuthorIce accretion-
dc.subject.keywordAuthorCoarray-
dc.subject.keywordAuthorParallel computation-
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