Publication:
Rocket Engine with Continuously Rotating Liquid-Film Detonation

dc.contributor.authorGusev, P. A.
dc.contributor.authorZelensky, V. A.
dc.contributor.authorEvstratov, E. V.
dc.contributor.authorAlymov, M. I.
dc.contributor.authorFrolov, S. M.
dc.contributor.authorShamshin, I. O.
dc.contributor.authorAksenov, V. S.
dc.contributor.authorФролов, Сергей Михайлович
dc.contributor.authorАксенов, Виктор Серафимович
dc.date.accessioned2024-11-25T14:39:27Z
dc.date.available2024-11-25T14:39:27Z
dc.date.issued2020
dc.description.abstract© 2018, © 2018 Taylor & Francis. The possibility of organizing a continuous-detonation combustion of a liquid fuel film in an annular combustor of a detonation liquid-propellant rocket engine has been demonstrated. The near-limit mode of the longitudinally pulsating “film” detonation and the continuous spinning “film” detonation modes with one and two detonation waves circulating in the annular gap of the combustor are recorded in the fire tests.
dc.format.extentС. 144-165
dc.identifier.citationRocket Engine with Continuously Rotating Liquid-Film Detonation / Gusev, P.A. [et al.] // Combustion Science and Technology. - 2020. - 192. - № 1. - P. 144-165. - 10.1080/00102202.2018.1557643
dc.identifier.doi10.1080/00102202.2018.1557643
dc.identifier.urihttps://www.doi.org/10.1080/00102202.2018.1557643
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dc.identifier.urihttp://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcAuth=Alerting&SrcApp=Alerting&DestApp=WOS_CPL&DestLinkType=FullRecord&UT=WOS:000508354300008
dc.identifier.urihttps://openrepository.mephi.ru/handle/123456789/19966
dc.relation.ispartofCombustion Science and Technology
dc.titleRocket Engine with Continuously Rotating Liquid-Film Detonation
dc.typeArticle
dspace.entity.typePublication
oaire.citation.issue1
oaire.citation.volume192
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