Studie vlivu vrtulového proudu na křídlo u nekonvenčních uspořádání pohonných jednotek
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Date
Authors
Hazman, Yagmur
Advisor
Referee
Mark
C
Journal Title
Journal ISSN
Volume Title
Publisher
Vysoké učení technické v Brně. Fakulta strojního inženýrství
ORCID
Abstract
Today'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.
Today'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.
Today'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.
Description
Citation
HAZMAN, Y. Studie vlivu vrtulového proudu na křídlo u nekonvenčních uspořádání pohonných jednotek [online]. Brno: Vysoké učení technické v Brně. Fakulta strojního inženýrství. 2022.
Document type
Document version
Date of access to the full text
Language of document
en
Study field
bez specializace
Comittee
doc. 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)
Date of acceptance
2022-06-20
Defence
The 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.
Result of defence
práce byla úspěšně obhájena