Tests of the propulsion unit of an unconventional ultralight aircraft

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F13%3A00213934" target="_blank" >RIV/68407700:21220/13:00213934 - isvavai.cz</a>
Result on the web
<a href="http://stc.fs.cvut.cz/history/2013/sbornik/papers/pdf/2585.pdf?_=1364843497" target="_blank" >http://stc.fs.cvut.cz/history/2013/sbornik/papers/pdf/2585.pdf?_=1364843497</a>
DOI - Digital Object Identifier
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Result language
angličtina
Original language name
Tests of the propulsion unit of an unconventional ultralight aircraft
Original language description
This paper deals with static tests of the demonstrator of a new engine for the category of ultralight and small sport aircraft. Used laboratory stand for the fan drive allows the comparison of different construction solutions. The purpose of these testswas to verify the functionality of the drive, the measurement procedure and to compare the individual obtained propulsion system results. Realized experiments focused primarily on determining the available thrust of the new engine, its dependence on theengine speed, the view of the velocity field in the output of air duct while at the same time ensuring the necessary cooling of the engine and data acquisition for subsequent design optimization.
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

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