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헬리콥터 휠타입 착륙장치 충돌특성 연구

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dc.contributor.author박효근-
dc.contributor.author김동만-
dc.contributor.author김동현-
dc.contributor.author조윤모-
dc.contributor.author정재훈-
dc.date.accessioned2022-12-27T06:23:36Z-
dc.date.available2022-12-27T06:23:36Z-
dc.date.issued2008-
dc.identifier.issn1598-9127-
dc.identifier.issn2636-0640-
dc.identifier.urihttps://scholarworks.gnu.ac.kr/handle/sw.gnu/27773-
dc.description.abstractIn this study, the dynamic characteristics for the wheel-type landing gear system of helicopter have been analyzed. Nonlinear multi-body dynamic models of the landing gear system are constructed and the equations of motion, kinematics and internal forces of shock strut are considered. In addition, flexibility effect of the wheel axle with equivalent beam element is taken into account. General purpose commercial finite code, SAMCEF which includes MECANO module is applied. The results of dynamic simulation for various landing and weight conditions are presented and compared with each other. Based on the results, characteristics of impact dynamic behaviors of the landing gear system are practically investigated.-
dc.format.extent11-
dc.language한국어-
dc.language.isoKOR-
dc.publisher한국군사과학기술학회-
dc.title헬리콥터 휠타입 착륙장치 충돌특성 연구-
dc.title.alternativeImpact Dynamic Analysis for the Wheel-Type Landing Gear System of Helicopter-
dc.typeArticle-
dc.publisher.location대한민국-
dc.identifier.bibliographicCitation한국군사과학기술학회지, v.11, no.5, pp 12 - 22-
dc.citation.title한국군사과학기술학회지-
dc.citation.volume11-
dc.citation.number5-
dc.citation.startPage12-
dc.citation.endPage22-
dc.identifier.kciidART001290169-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClasskci-
dc.subject.keywordAuthorWheel-Type Landing Gear(휠타입 착륙장치)-
dc.subject.keywordAuthorNose Landing Gear(전륜착륙장치)-
dc.subject.keywordAuthorMain Landing Gear(주륜착륙장치)-
dc.subject.keywordAuthorNonlinear Multi-body Dynamics(비선형 다물체 동역학)-
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