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Development of numerical simulation software for hybrid rocket engines' performance studies

dc.contributor.advisorBrojo, Francisco Miguel Ribeiro Proença
dc.contributor.authorAmaro, Telmo
dc.date.accessioned2015-06-25T14:43:29Z
dc.date.available2015-06-25T14:43:29Z
dc.date.issued2009
dc.date.submitted2009-08
dc.description.abstractA numerical simulation software was developed for Hybrid Rocket Engines' performance studies. Two-dimensional gas flow, mass fraction and regression rate functions were developed and tested with H2 engine geometry. Program structure was prepared to determine three-dimensional gas flows, combustion characteristics and thrust curves.por
dc.identifier.urihttp://hdl.handle.net/10400.6/3626
dc.language.isoengpor
dc.titleDevelopment of numerical simulation software for hybrid rocket engines' performance studiespor
dc.typemaster thesis
dspace.entity.typePublication
rcaap.rightsopenAccesspor
rcaap.typemasterThesispor
thesis.degree.disciplineEngenharia Aeronáuticapor
thesis.degree.levelMestrepor
thesis.degree.nameDissertação apresentada à Universidade da Beira Interior para a obtenção do grau de mestre em Engenharia Aeronáuticapor

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