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Universidade de Brasília
Use este identificador para citar ou linkar para este item: http://repositorio.unb.br/handle/10482/35909
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dc.contributor.authorLee, Jungpyo-
dc.contributor.authorRhee, Sunjae-
dc.contributor.authorKim, Jinkon-
dc.contributor.authorMoon, Heejang-
dc.contributor.authorShynkarenko, Olexiy-
dc.contributor.authorSimone, Domenico-
dc.contributor.authorMorita, Takakazu-
dc.date.accessioned2019-12-02T13:26:29Z-
dc.date.available2019-12-02T13:26:29Z-
dc.date.issued2019-
dc.identifier.citationLEE, Jungpyo et al. Combustion instability for hybrid rocket motors with a diaphragm. In: EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES, 8., 2019, Madrid. Proceedings [...]. Madrid: EUCASS association, 2019. DOI: 10.13009/EUCASS2019-462. Disponível em: https://www.eucass.eu/index.php/conferences-and-publications/search-in-publications?searchword=eucass/2019&searchphrase=all&limit=20&areas[0]=doc_indexer&start=240. Acesso em: 02 dez. 2019.pt_BR
dc.identifier.urihttps://repositorio.unb.br/handle/10482/35909-
dc.language.isoInglêspt_BR
dc.publisherEUCASS associationpt_BR
dc.rightsAcesso Restritopt_BR
dc.titleCombustion instability for hybrid rocket motors with a diaphragmpt_BR
dc.typeTrabalhopt_BR
dc.subject.keywordMotores de foguetespt_BR
dc.subject.keywordCâmaras de combustãopt_BR
dc.identifier.doi10.13009/EUCASS2019-462pt_BR
dc.relation.publisherversionhttps://www.eucass.eu/index.php/conferences-and-publications/search-in-publications?searchword=eucass/2019&searchphrase=all&limit=20&areas[0]=doc_indexer&start=240pt_BR
dc.description.abstract1A diaphragm has been used to enhance fuel regression rate and combustion efficiency in hybrid rockets. On the other hand, it has been observed that significant pressure oscillations occurred. In this paper, main factor on the excitation of the instability was studied. Lab-scale firing tests considering the various experimental conditions, such as the diaphragm location and diameter, were conducted, and combustion visualization tests were performed to confirm the instability mechanism. The excitation source of the pressure oscillations was the edge-tone instability. Finally, a new grain which had high regression rate and also was stable combustion was proposed.pt_BR
dc.rights.holderCopyright © 2019 by First Author and Second Author. Published by the EUCASS association with permission.-
dc.description.unidadeFaculdade UnB Gama (FGA)-
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