About: Tests of the propulsion unit of an unconventional ultralight aircraft

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An Entity of Type : http://linked.opendata.cz/ontology/domain/vavai/Vysledek, within Data Space : linked.opendata.cz associated with source document(s)

Attributes	Values
rdf:type	skos:Concept http://linked.opendata.cz/ontology/domain/vavai/Vysledek
rdfs:seeAlso	http://stc.fs.cvut.cz/history/2013/sbornik/papers/pdf/2585.pdf?_=1364843497
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 tests was 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 the engine 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. 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 tests was 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 the engine 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. (en)
Title	Tests of the propulsion unit of an unconventional ultralight aircraft Tests of the propulsion unit of an unconventional ultralight aircraft (en)
skos:prefLabel	Tests of the propulsion unit of an unconventional ultralight aircraft Tests of the propulsion unit of an unconventional ultralight aircraft (en)
skos:notation	RIV/68407700:21220/13:00213934!RIV14-MPO-21220___
http://linked.open...avai/riv/aktivita	P
http://linked.open...avai/riv/aktivity	P(FR-TI3/527)
http://linked.open...vai/riv/dodaniDat	2014
http://linked.open...aciTvurceVysledku	Helmich, Martin Janko, Luboš
http://linked.open.../riv/druhVysledku	D - Článek ve sborníku
http://linked.open...iv/duvernostUdaju	S - Úplné a pravdivé údaje nepodléhající ochraně podle zvláštních právních předpisů
http://linked.open...titaPredkladatele	České vysoké učení technické v Praze / Fakulta strojní
http://linked.open...dnocenehoVysledku	110730
http://linked.open...ai/riv/idVysledku	RIV/68407700:21220/13:00213934
http://linked.open...riv/jazykVysledku	eng - angličtina
http://linked.open.../riv/klicovaSlova	Propulsion unit; laboratory stand fan drive; static thrust; available thrust (en)
http://linked.open.../riv/klicoveSlovo	available thrust laboratory stand fan drive Propulsion unit static thrust
http://linked.open...ontrolniKodProRIV	[4B4377EAD99E]
http://linked.open...v/mistoKonaniAkce	Praha
http://linked.open...i/riv/mistoVydani	Praha
http://linked.open...i/riv/nazevZdroje	Studentská tvůrčí činnost 2013
http://linked.open...in/vavai/riv/obor	JT
http://linked.open...ichTvurcuVysledku	2 (xsd:int)
http://linked.open...cetTvurcuVysledku	2 (xsd:int)
http://linked.open...vavai/riv/projekt	*Ducted Fan Ultralight Aircraft
http://linked.open...UplatneniVysledku	2013
http://linked.open...iv/tvurceVysledku	Helmich, Martin Janko, Luboš
http://linked.open...vavai/riv/typAkce	EUR - Evropská
http://linked.open.../riv/zahajeniAkce	2013-04-09 (xsd:date)
number of pages	14 (xsd:int)
http://purl.org/ne...btex#hasPublisher	České vysoké učení technické v Praze. Fakulta strojní
https://schema.org/isbn	978-80-01-05232-7
http://localhost/t...ganizacniJednotka	21220

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