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Computational elements for high-fidelity aerodynamic analysis and design optimisation

DC Field Value Language
dc.contributor.authorKim, Chongam-
dc.creator김종암-
dc.date.accessioned2013-04-23T02:02:03Z-
dc.date.available2013-04-23T02:02:03Z-
dc.date.issued2010-11-
dc.identifier.citationDEFENCE SCIENCE JOURNAL Vol.60 No.6, pp. 628-638-
dc.identifier.issn0011-748X-
dc.identifier.urihttps://hdl.handle.net/10371/82300-
dc.description.abstractThe study reviews the role of computational fluid dynamics (CFD) in aerodynamic shape optimisation,
and discusses some of the efficient design methodologies. The article in the first part, numerical schemes
required for high-fidelity aerodynamic flow analysis are discussed. To accurately resolve high-speed flow
physics, high-fidelity shock-stable schemes as well as intelligent limiting strategy mimicking multi-dimensional
flow physics are essential. Exploiting these numerical schemes, some applications for 3-D internal/external
flow analyses were carried out with various grid systems which enable the treatment of complex geometries.
In the second part, depending on the number of design variables and the way to obtain sensitivities or design
points, several global and local optimisation methods for aerodynamic shape optimisation are discussed. To
avoid the problem that solutions of gradient-based optimisation method, (GBOM) are often trapped in local
optimum, remedy by combining GBOM with global optimum strategy, such as surrogate models and genetic
algorithm (GA) has been examined. As an efficient grid deformation tool, grid deformation technique using
NURBS function is discussed. Lastly, some 3-D examples for aerodynamic shape optimisation works based
on the proposed design methodology are presented.
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dc.language.isoenen
dc.publisherDEFENCE SCIENTIFIC INFORMATION DOCUMENTATION CENTREen
dc.subject복합학en
dc.subjectAerodynamic shape optimisation-
dc.subjecthigh-fidelity numerical methods-
dc.subjectgradient-based optimisation method-
dc.subjectmeta modelling-
dc.subjectgenetic algorithm-
dc.subjectadjoint variable method-
dc.subjectaerodynamic analysis-
dc.titleComputational elements for high-fidelity aerodynamic analysis and design optimisationen
dc.typeArticle-
dc.contributor.AlternativeAuthor김종암-
dc.description.srndOAIID:oai:osos.snu.ac.kr:snu2010-01/102/0000004648/3-
dc.description.srndSEQ:3-
dc.description.srndPERF_CD:SNU2010-01-
dc.description.srndEVAL_ITEM_CD:102-
dc.description.srndUSER_ID:0000004648-
dc.description.srndADJUST_YN:N-
dc.description.srndEMP_ID:A001138-
dc.description.srndDEPT_CD:446-
dc.description.srndCITE_RATE:.304-
dc.description.srndFILENAME:Computational Elements for High-Fidelity Aerodynamic Analysis and Design Optimisation.pdf-
dc.description.srndDEPT_NM:기계항공공학부-
dc.description.srndEMAIL:chongam@snu.ac.kr-
dc.description.srndSCOPUS_YN:Y-
dc.description.srndCONFIRM:Y-
dc.identifier.srnd2010-01/102/0000004648/3-
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