Static Tests of Unconventional Propulsion Units for Ultralight Airplanes

Result code in IS VaVaI
<a href="https://www.isvavai.cz/riv?ss=detail&h=RIV%2F68407700%3A21220%2F14%3A00218694" target="_blank" >RIV/68407700:21220/14:00218694 - isvavai.cz</a>
Result on the web
<a href="https://ojs.cvut.cz/ojs/index.php/ap/article/view/AP.2014.54.0183" target="_blank" >https://ojs.cvut.cz/ojs/index.php/ap/article/view/AP.2014.54.0183</a>
DOI - Digital Object Identifier
<a href="http://dx.doi.org/10.14311/AP.2014.54.0183" target="_blank" >10.14311/AP.2014.54.0183</a>

Result language
angličtina
Original language name
Static Tests of Unconventional Propulsion Units for Ultralight Airplanes
Original language description
This paper presents static tests of a new unconventional propulsion unit for small aviation airplanes. Our laboratory stand ? a fan drive demonstrator ? enables us to compare various design options. We performed experiments to verify the propulsion functionality and a measurement procedure to determine the available thrust of the propulsion unit and its dependence on engine speed. The results used for subsequent optimization include the operating parameters of the propulsion unit, and the temperature and velocity fields in parts of the air duct.
Czech name
—
Czech description
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Type
J<sub>x</sub> - Unclassified - Peer-reviewed scientific article (Jimp, Jsc and Jost)
CEP classification
JT - Propulsion, engines and fuels
OECD FORD branch
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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
2014
Confidentiality
S - Úplné a pravdivé údaje o projektu nepodléhají ochraně podle zvláštních právních předpisů

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