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dc.contributor.authorLema, Marcos
dc.contributor.authorGosset, Anne
dc.contributor.authorLópez Peña, Fernando
dc.contributor.authorSteelant, Johan
dc.date.accessioned2024-01-18T16:47:03Z
dc.date.available2024-01-18T16:47:03Z
dc.date.issued2022-10-07
dc.identifier.citationLema, M., Gosset, A., López Peña, F., and Steelant, J., “Liquid Column Separation Due to Fluid Hammer Occurrence in Propellant Lines,” Journal of Propulsion and Power, Vol. 39, No. 1, 2023, pp. 121–129. https://doi.org/10.2514/1.B38451es_ES
dc.identifier.issn1533-3876
dc.identifier.urihttp://hdl.handle.net/2183/34990
dc.descriptionThis version of the article has been accepted for publication, after peer review, but is not the Version of Record and does not reflect post-acceptance improvements, or any corrections. The Version of Record is available online at: https://doi.org/10.2514/1.B38451es_ES
dc.description.abstract[Abstract]: When a pressurized liquid enters a pipeline with a closed-end and under vacuum conditions, the resulting liquid front suddenly is brought to rest at the end of the pipe. This type of flow configuration is found in propulsion systems of satellites during priming operation and induces a fluid hammer followed by a column separation, generating a multiphase gas/vapor bubble. This paper aims at explaining the column separation mechanism by solving the momentum equation for the liquid column moving in the pipeline when column separation occurs, and by applying the integral form of the conservation principles to expansion and compression waves within the flow. The resulting model provides the velocity and position of the liquid front during column separation. Thus, the size and duration of the multiphase bubble can be determined, and the variables involved in the process are identified, which helps on the analysis of applications where this complex phenomenon is involved. It is shown that the initial velocity of the liquid front during column separation is the main parameter, which itself is a function of the fuel tank pressure and the fluid hammer pressure rise. The comparison of the predictions with experimental data shows an excellent agreement.es_ES
dc.description.sponsorshipThis research was supported by the Xunta de Galicia and the European Regional Development Funds under grant EDC431C-2021/39 and the Spanish Science and Education Ministry through grant RTI2018-101114-B-I00. We wish to acknowledge the support received from the Centro de Investigación de Galicia, funded by Xunta de Galicia and the European Regional Development Fund Galicia 2014–2020 Program through grant ED431G 2019/01. The present research activity was promoted by the European Space Research and Technology Centre of the European Space Agency through the General Support Technology Programme (GSTP) activity AO/1-6210/09/NL/CP.es_ES
dc.description.sponsorshipXunta de Galicia; EDC431C-2021/39es_ES
dc.description.sponsorshipXunta de Galicia; ED431G 2019/01es_ES
dc.language.isoenges_ES
dc.publisherAmerican Institute of Aeronautics and Astronauticses_ES
dc.relationInfo:eu-repo/grantAgreement/AEI/Plan Estatal de Investigación Científica y Técnica y de Innovación 2017-2020/RTI2018-101114-B-I00/ES/ ARQUITECTURA COGNITIVA PARA ROBOTS CON ADAPTACION DE COMPORTAMIENTO AUTONOMAMENTE MOTIVADAes_ES
dc.relation.urihttps://doi.org/10.2514/1.B38451es_ES
dc.rights© 2022 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-3876 to initiate your request. See also AIAA Rights and Permissions www.aiaa.org/randpes_ES
dc.subjectPropellantes_ES
dc.subjectSatelliteses_ES
dc.subjectPropulsion systemes_ES
dc.subjectVapour pressurees_ES
dc.subjectTait equationes_ES
dc.subjectMoody diagrames_ES
dc.subjectFluid structure interactiones_ES
dc.subjectSurface tensiones_ES
dc.subjectUnsteady flowses_ES
dc.subjectShear stresses_ES
dc.titleLiquid column separation due to fluid hammer occurrence in propellant lineses_ES
dc.typeinfo:eu-repo/semantics/articlees_ES
dc.rights.accessinfo:eu-repo/semantics/openAccesses_ES
UDC.journalTitleJournal of Propulsion and Poweres_ES
UDC.volume39es_ES
UDC.issue1es_ES
UDC.startPage121es_ES
UDC.endPage129es_ES
dc.identifier.doihttps://doi.org/10.2514/1.B38451


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