허니컴 샌드위치 패널 인서트의 충격파 전달 특성에 관한 실험 및 해석적 연구 Experimental and Analytical Study on Shock Wave Transfer Characteristic of Honeycomb Sandwich Panel Insert

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dc.contributor.author박현수ko
dc.contributor.author황대현ko
dc.contributor.author한재흥ko
dc.date.accessioned2019-06-28T04:50:02Z-
dc.date.available2019-06-28T04:50:02Z-
dc.date.created2019-06-28-
dc.date.created2019-06-28-
dc.date.issued2019-06-
dc.identifier.citation한국소음진동공학회논문집, v.29, no.3, pp.389 - 395-
dc.identifier.issn1598-2785-
dc.identifier.urihttp://hdl.handle.net/10203/262843-
dc.description.abstractSevere pyroshock can cause failure of mounted electronic equipment used in various space missions. To prevent this problem, it is important to predict the propagation path and attenuation of shock in space structures. In the case of a honeycomb sandwich panel, which is widely used in satellites, an insert is used in essential to connect with other structures and the shock wave propagates through this insert system. In this study, the shock attenuation performance of a honeycomb sandwich panel insert system is measured by a shock propagation experiment. Modeling and finite element analysis techniques for such a honeycomb sandwich panel with an insert system are introduced. The results of the experiment and analysis are compared.-
dc.languageKorean-
dc.publisher한국소음진동공학회-
dc.title허니컴 샌드위치 패널 인서트의 충격파 전달 특성에 관한 실험 및 해석적 연구-
dc.title.alternativeExperimental and Analytical Study on Shock Wave Transfer Characteristic of Honeycomb Sandwich Panel Insert-
dc.typeArticle-
dc.type.rimsART-
dc.citation.volume29-
dc.citation.issue3-
dc.citation.beginningpage389-
dc.citation.endingpage395-
dc.citation.publicationname한국소음진동공학회논문집-
dc.identifier.kciidART002473248-
dc.contributor.localauthor한재흥-
dc.description.isOpenAccessN-
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AE-Journal Papers(저널논문)
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