A Measuring Stand for a Ducted Fan Aircraft Propulsion Unit

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F13%3A00214455" target="_blank" >RIV/68407700:21220/13:00214455 - isvavai.cz</a>
Result on the web
<a href="http://www.epj-conferences.org" target="_blank" >http://www.epj-conferences.org</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
A Measuring Stand for a Ducted Fan Aircraft Propulsion Unit
Original language description
The UL-39 ultra-light aircraft which is being developed by the Department of Aerospace Engineering, Faculty of Mechanical Engineering, Czech Technical University in Prague, is equipped with an unconventional ducted fan propulsion unit. The unit consistsof an axial fan driven by a piston engine and placed inside a duct ended with a nozzle. This article describes the arrangement of a modernised measuring stand for this highly specific propulsion unit which will be able to measure the fan pressure ratio and velocity field in front of and behind the fan and its characteristic curve.
Czech name
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Czech description
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Project
<a href="/en/project/FR-TI3%2F527" target="_blank" >FR-TI3/527: Ducted Fan Ultralight Aircraft</a><br>
Continuities
P - Projekt vyzkumu a vyvoje financovany z verejnych zdroju (s odkazem do CEP)

Publication year
2013
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

Article name in the collection
Proceedings of the International Conference Experimental Fluid Mechanics 2013
ISBN
978-80-260-5375-0
ISSN
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e-ISSN
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Number of pages
8
Pages from-to
253-260
Publisher name
Technical University of Liberec
Place of publication
Liberec
Event location
Kutná Hora
Event date
Nov 19, 2013
Type of event by nationality
CST - Celostátní akce
UT code for WoS article
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