A trended Kriging model with R-2 indicator and application to design optimization

Cited 15 time in webofscience Cited 0 time in scopus
  • Hit : 325
  • Download : 0
DC FieldValueLanguage
dc.contributor.authorKwon, Hyungilko
dc.contributor.authorChoi, Seongimko
dc.date.accessioned2015-11-20T08:57:58Z-
dc.date.available2015-11-20T08:57:58Z-
dc.date.created2015-07-21-
dc.date.created2015-07-21-
dc.date.issued2015-06-
dc.identifier.citationAEROSPACE SCIENCE AND TECHNOLOGY, v.43, pp.111 - 125-
dc.identifier.issn1270-9638-
dc.identifier.urihttp://hdl.handle.net/10203/200908-
dc.description.abstractA trended Kriging model is known to improve the overall accuracy and efficiency of surrogate modeling; however, most studies have focused on a non-trended Kriging model because of the difficulty in the identification of a trend from an unknown data set. In the present study, an R-2 indicator for a Kriging surrogate model has been developed to identify the trend from a training data set. Both linear and nonlinear trends are identified with the R-2 indicator using the function analytic values and the function derivatives of the Kriging predictor. The trends identified by the indicator are used to determine the order of the drift function in the trended Kriging model. A trend identification of the Kriging model was validated with various analytic test functions. Subsequently, more practical uses of the R-2 indicator applied to actual responses from the Computational Fluid Dynamics (CFD) analysis of transonic airfoil. In Conclusion, the trended Kriging model can improve overall accuracy of responses if the maximum order of drift function is properly adjusted to the trend of sample space identified by the R-2 indicator.-
dc.languageEnglish-
dc.publisherELSEVIER FRANCE-EDITIONS SCIENTIFIQUES MEDICALES ELSEVIER-
dc.subjectCOMPUTER EXPERIMENTS-
dc.subjectALGORITHM-
dc.titleA trended Kriging model with R-2 indicator and application to design optimization-
dc.typeArticle-
dc.identifier.wosid000356754300012-
dc.identifier.scopusid2-s2.0-84924809233-
dc.type.rimsART-
dc.citation.volume43-
dc.citation.beginningpage111-
dc.citation.endingpage125-
dc.citation.publicationnameAEROSPACE SCIENCE AND TECHNOLOGY-
dc.identifier.doi10.1016/j.ast.2015.02.021-
dc.contributor.nonIdAuthorChoi, Seongim-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorKriging surrogate model-
dc.subject.keywordAuthorTrend indicator-
dc.subject.keywordAuthorCoefficient of determination-
dc.subject.keywordAuthorComputational fluid dynamics-
dc.subject.keywordAuthorDesign optimization-
dc.subject.keywordPlusCOMPUTER EXPERIMENTS-
dc.subject.keywordPlusALGORITHM-
Appears in Collection
Files in This Item
There are no files associated with this item.
This item is cited by other documents in WoS
⊙ Detail Information in WoSⓡ Click to see webofscience_button
⊙ Cited 15 items in WoS Click to see citing articles in records_button

qr_code

  • mendeley

    citeulike


rss_1.0 rss_2.0 atom_1.0