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dc.contributor.author최동훈-
dc.date.accessioned2018-03-12T06:30:59Z-
dc.date.available2018-03-12T06:30:59Z-
dc.date.issued2013-05-
dc.identifier.citation한국항공우주학회지, 2013, 41(5), P.404-414en_US
dc.identifier.issn1225-1348-
dc.identifier.issn2287-6871-
dc.identifier.urihttp://click.ndsl.kr/servlet/LinkingDetailView?cn=JAKO201319947249485&dbt=JAKO&org_code=O483&site_code=SS1483&service_code=01-
dc.identifier.urihttp://hdl.handle.net/20.500.11754/45438-
dc.description.abstract전투기의 개념설계 과정에서는 기준형상 도출을 위해 비교분석연구가 반복된다. 반복적인 비교분석연구가 자동화되면 효율적으로 기준형상을 도출할 수 있다. 본 연구에서는 비교분석연구의 자동화를 위한 성능해석 프로그램을 개발했다. 프로그램은 형상생성모듈과 중량예측모듈, 임무성능 해석모듈로 구성된다. 형상생성모듈을 사용하여 3D CAD 모델 생성이 가능하며 중량예측모듈에서는 경험식을 사용하여 중량을 예측한다. 임의의 임무형상에 대한 임무성능 해석이 가능하며 최적화 기법을 사용하여 최적 임무성능 계산이 가능하다. 개발된 프로그램의 검증을 진행하여 개념설계 단계에 적용 가능함을 확인했다.In the conceptual design phase of jet fighters, the trade study is performed repeatedly for a selection of the baseline configuration. The automation of repeated trade study makes possible to select efficiently the baseline configuration. In this study, the performance analysis code was developed for the automation of trade study. The code was consists of the module of shape generation, the module of weight estimation, the module of mission performance analysis. 3D CAD Model can be generated by the module of shape generation and Weight can be estimated by using the empirical equation in the module of weight estimation. The module of mission performance analysis was able to calculate the mission performance about the arbitrary mission profile. In addition, the optimal mission performance can be calculated by using optimization method. By performing the validation, the code was confirmed to be able to apply to the conceptual design phase.en_US
dc.language.isoko_KRen_US
dc.publisher한국항공우주학회en_US
dc.subject성능해석en_US
dc.subject개념설계en_US
dc.subject중량예측en_US
dc.subject임무형상en_US
dc.subject점진적 2차 반응표면법en_US
dc.title전투기의 개념설계를 위한 성능해석 프로그램 개발en_US
dc.typeArticleen_US
dc.relation.no5-
dc.relation.volume41-
dc.identifier.doi10.5139/JKSAS.2013.41.5.404-
dc.relation.page404-414-
dc.relation.journal한국항공우주학회지-
dc.contributor.googleauthor김태우-
dc.contributor.googleauthor최현민-
dc.contributor.googleauthor최병렬-
dc.contributor.googleauthor이성진-
dc.contributor.googleauthor남화진-
dc.contributor.googleauthor최동훈-
dc.contributor.googleauthor조진수-
dc.contributor.googleauthorKim, Taewoo-
dc.contributor.googleauthorChoi, Hyunmin-
dc.contributor.googleauthorChoi, Byungryul-
dc.contributor.googleauthorLee, Sungjin-
dc.contributor.googleauthorNam, Hwajin-
dc.contributor.googleauthorChoi, Donghoon-
dc.contributor.googleauthorCho, Jinsoo-
dc.relation.code2012210721-
dc.sector.campusS-
dc.sector.daehakCOLLEGE OF ENGINEERING[S]-
dc.sector.departmentDIVISION OF MECHANICAL ENGINEERING-
dc.identifier.piddhchoi-
Appears in Collections:
COLLEGE OF ENGINEERING[S](공과대학) > MECHANICAL ENGINEERING(기계공학부) > Articles
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