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비정상 Adjoint Variable 기법을 이용한 날갯짓 익형의 최적설계 : Flapping airfoil optimization design using unsteady adjoint variable method

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dc.contributor.advisor김종암-
dc.contributor.author이상호-
dc.date.accessioned2010-05-10T03:46:56Z-
dc.date.available2010-05-10T03:46:56Z-
dc.date.copyright2005.-
dc.date.issued2005-
dc.identifier.urihttp://dcollection.snu.ac.kr:80/jsp/common/DcLoOrgPer.jsp?sItemId=000000051137kog
dc.identifier.urihttps://hdl.handle.net/10371/64825-
dc.description학위논문(석사)--서울대학교 대학원 :항공우주공학과,2005.ko
dc.format.extentvi, 53 장ko
dc.language.isokoko
dc.publisher서울대학교 대학원ko
dc.subject공력 최적화ko
dc.subjectOptimizationko
dc.subject비정상 Adjoint Variable Methodko
dc.subjectUnsteady Adjoint Variable Methodko
dc.subjectTerminal boundary condtionko
dc.title비정상 Adjoint Variable 기법을 이용한 날갯짓 익형의 최적설계ko
dc.title.alternativeFlapping airfoil optimization design using unsteady adjoint variable methodko
dc.typeThesis-
dc.contributor.department항공우주공학과-
dc.description.degreeMasterko
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