자동미분의 공력최적설계 적용Application of the Automatic Differentiation to Aerodynamic Design Optimization
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | 이재훈 | - |
| dc.contributor.author | 김수환 | - |
| dc.contributor.author | 안중기 | - |
| dc.contributor.author | 권장혁 | - |
| dc.date.accessioned | 2013-03-18T19:52:29Z | - |
| dc.date.available | 2013-03-18T19:52:29Z | - |
| dc.date.created | 2012-02-06 | - |
| dc.date.issued | 2004-10 | - |
| dc.identifier.citation | 한국전산유체공학회 학술대회, v., no., pp.181 - 186 | - |
| dc.identifier.uri | http://hdl.handle.net/10203/151896 | - |
| dc.description.abstract | In gradient based optimization methods, the finite differencing which uses small perturbations in the design variables has been used to calculate the sensitivity. Recently, the automatic differentiation has been widely studied to calculate the function value and the sensitivities simultaneously. In this paper, the applicability of the automatic differentiation In the aerodynamic design optimization is studied. ADIFOR and TAPENADE are used to generate the codes which give the function value and the sensitivities for 2D compressible inviscid flows. | - |
| dc.language | KOR | - |
| dc.publisher | 한국전산유체공학회 | - |
| dc.title | 자동미분의 공력최적설계 적용 | - |
| dc.title.alternative | Application of the Automatic Differentiation to Aerodynamic Design Optimization | - |
| dc.type | Conference | - |
| dc.type.rims | CONF | - |
| dc.citation.beginningpage | 181 | - |
| dc.citation.endingpage | 186 | - |
| dc.citation.publicationname | 한국전산유체공학회 학술대회 | - |
| dc.identifier.conferencecountry | South Korea | - |
| dc.identifier.conferencecountry | South Korea | - |
| dc.contributor.localauthor | 권장혁 | - |
| dc.contributor.nonIdAuthor | 이재훈 | - |
| dc.contributor.nonIdAuthor | 김수환 | - |
| dc.contributor.nonIdAuthor | 안중기 | - |
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