Studie vlivu vrtulového proudu na křídlo u nekonvenčních uspořádání pohonných jednotek

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but.committeedoc. Ing. Ivo Jebáček, Ph.D. (předseda) doc. Ing. Jiří Hlinka, Ph.D. (místopředseda) doc. Ing. Jaroslav Juračka, Ph.D. (člen) Ing. Robert Popela, Ph.D. (člen) Ing. Miroslav Šplíchal, Ph.D. (člen)cs
but.defenceThe student gave the presentation of her thesis. Evaluation of the supervisor and the reviewer were read and opponent's question which the student answered. In the discussion, initial comments and questions were related to the presentation, graphics. Further discussion was about the wing tunnel measurement used as reference to calculations in the thesis, electric propulsion. Student answered well.cs
but.jazykangličtina (English)
but.programAerospace Technologycs
but.resultpráce byla úspěšně obhájenacs
dc.contributor.advisorNavrátil, Janen
dc.contributor.authorHazman, Yagmuren
dc.contributor.refereeGrim, Roberten
dc.date.created2022cs
dc.description.abstractToday's aircraft propulsion development is moving towards the use of electric power units. One possibility is the use of distributed propulsion, i.e., several independent power units located on the wing. An example is the NASA X-57 Maxwell experimental aircraft. This thesis focuses on the study of the effect of this unconventional propulsion configuration on the aerodynamic performance of the aircraft.en
dc.description.abstractToday's aircraft propulsion development is moving towards the use of electric power units. One possibility is the use of distributed propulsion, i.e., several independent power units located on the wing. An example is the NASA X-57 Maxwell experimental aircraft. This thesis focuses on the study of the effect of this unconventional propulsion configuration on the aerodynamic performance of the aircraft.cs
dc.description.markCcs
dc.identifier.citationHAZMAN, Y. Studie vlivu vrtulového proudu na křídlo u nekonvenčních uspořádání pohonných jednotek [online]. Brno: Vysoké učení technické v Brně. Fakulta strojního inženýrství. 2022.cs
dc.identifier.other140203cs
dc.identifier.urihttp://hdl.handle.net/11012/207176
dc.language.isoencs
dc.publisherVysoké učení technické v Brně. Fakulta strojního inženýrstvícs
dc.rightsStandardní licenční smlouva - přístup k plnému textu bez omezenícs
dc.subjectNASA X-57 Maxwellen
dc.subjectCFDen
dc.subjectANSAen
dc.subjectFluenten
dc.subjectLow-Speed Wind Tunnelen
dc.subjectUnconventional Propulsionen
dc.subjectPropeller Slipstreamen
dc.subjectActuator Disk.en
dc.subjectNASA X-57 Maxwellcs
dc.subjectCFDcs
dc.subjectANSAcs
dc.subjectFluentcs
dc.subjectLow-Speed Wind Tunnelcs
dc.subjectUnconventional Propulsioncs
dc.subjectPropeller Slipstreamcs
dc.subjectActuator Disk.cs
dc.titleStudie vlivu vrtulového proudu na křídlo u nekonvenčních uspořádání pohonných jednoteken
dc.title.alternativeStudy of propeller slipstream influence on the wing with unconventional configuration of propulsion systemcs
dc.typeTextcs
dc.type.drivermasterThesisen
dc.type.evskpdiplomová prácecs
dcterms.dateAccepted2022-06-20cs
dcterms.modified2022-06-22-13:51:23cs
eprints.affiliatedInstitution.facultyFakulta strojního inženýrstvícs
sync.item.dbid140203en
sync.item.dbtypeZPen
sync.item.insts2025.03.27 10:38:56en
sync.item.modts2025.01.15 17:29:16en
thesis.disciplinebez specializacecs
thesis.grantorVysoké učení technické v Brně. Fakulta strojního inženýrství. Letecký ústavcs
thesis.levelInženýrskýcs
thesis.nameIng.cs
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