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dc.contributorArbos Torrent, Sara
dc.contributorLizandra Dalmases, José Oriol
dc.contributor.authorMurnaghan Murnaghan, Murrough
dc.contributor.otherUniversitat Politècnica de Catalunya. Departament de Física
dc.date.accessioned2020-01-08T18:08:31Z
dc.date.available2020-01-08T18:08:31Z
dc.date.issued2019-06
dc.identifier.urihttp://hdl.handle.net/2117/174450
dc.description.abstractThis report outlines the pertinent theory and methods for supersonic nozzle design using the method of characteristics. The programmes developed design ideal nozzle contours, using numerical methods based on the gas properties, for desired exit velocities. Ideal contours include the most rapidexpansion without inducing shock waves followed by the straigh tening sec-tion to provide uniform exit conditions. Then based on the ideal results, thecontours can be truncated and the shape modified to induce minor shocksand only sacrifice minimal thrust to save length and thereby weight.
dc.language.isoeng
dc.publisherUniversitat Politècnica de Catalunya
dc.subjectÀrees temàtiques de la UPC::Aeronàutica i espai
dc.subject.lcshRockets (Aeronautics)--Nozzles
dc.subject.otherSupersonic nozzle design
dc.subject.othermethod of characteristics
dc.subject.othertruncated nozzle
dc.subject.otherideal nozzle contour
dc.titleStudy of minimum length, supersonic nozzle design using the Method of Characteristics
dc.typeMaster thesis
dc.subject.lemacCoets (Aeronàutica) -- Sistemes de propulsió
dc.identifier.slugPRISMA-147080
dc.rights.accessOpen Access
dc.date.updated2019-10-14T13:44:02Z
dc.audience.educationlevelMàster
dc.audience.mediatorEscola Superior d'Enginyeries Industrial, Aeroespacial i Audiovisual de Terrassa


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