Original title: Studie vlivu vrtulového proudu na křídlo u nekonvenčních uspořádání pohonných jednotek
Translated title: Study of propeller slipstream influence on the wing with unconventional configuration of propulsion system
Authors: Hazman, Yagmur ; Grim, Robert (referee) ; Navrátil, Jan (advisor)
Document type: Master’s theses
Year: 2022
Language: eng
Publisher: Vysoké učení technické v Brně. Fakulta strojního inženýrství
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.
Keywords: Actuator Disk.; ANSA; CFD; Fluent; Low-Speed Wind Tunnel; NASA X-57 Maxwell; Propeller Slipstream; Unconventional Propulsion; Actuator Disk.; ANSA; CFD; Fluent; Low-Speed Wind Tunnel; NASA X-57 Maxwell; Propeller Slipstream; Unconventional Propulsion

Institution: Brno University of Technology (web)
Document availability information: Fulltext is available in the Brno University of Technology Digital Library.
Original record: http://hdl.handle.net/11012/207176

Permalink: http://www.nusl.cz/ntk/nusl-586087


The record appears in these collections:
Universities and colleges > Public universities > Brno University of Technology
Academic theses (ETDs) > Master’s theses