This HTML5 document contains 42 embedded RDF statements represented using HTML+Microdata notation.

The embedded RDF content will be recognized by any processor of HTML5 Microdata.

Namespace Prefixes

PrefixIRI
n8http://linked.opendata.cz/ontology/domain/vavai/riv/typAkce/
dctermshttp://purl.org/dc/terms/
n20http://localhost/temp/predkladatel/
n10http://purl.org/net/nknouf/ns/bibtex#
n15http://linked.opendata.cz/resource/domain/vavai/riv/tvurce/
n17http://linked.opendata.cz/ontology/domain/vavai/
n14https://schema.org/
shttp://schema.org/
skoshttp://www.w3.org/2004/02/skos/core#
n3http://linked.opendata.cz/ontology/domain/vavai/riv/
n13http://linked.opendata.cz/resource/domain/vavai/vysledek/RIV%2F68407700%3A21260%2F14%3A00220451%21RIV15-MSM-21260___/
n2http://linked.opendata.cz/resource/domain/vavai/vysledek/
rdfhttp://www.w3.org/1999/02/22-rdf-syntax-ns#
n5http://linked.opendata.cz/ontology/domain/vavai/riv/klicoveSlovo/
n16http://linked.opendata.cz/ontology/domain/vavai/riv/duvernostUdaju/
xsdhhttp://www.w3.org/2001/XMLSchema#
n19http://linked.opendata.cz/ontology/domain/vavai/riv/aktivita/
n4http://linked.opendata.cz/ontology/domain/vavai/riv/jazykVysledku/
n12http://linked.opendata.cz/ontology/domain/vavai/riv/obor/
n6http://linked.opendata.cz/ontology/domain/vavai/riv/druhVysledku/
n7http://reference.data.gov.uk/id/gregorian-year/

Statements

Subject Item
n2:RIV%2F68407700%3A21260%2F14%3A00220451%21RIV15-MSM-21260___
rdf:type
skos:Concept n17:Vysledek
dcterms:description
This paper presents the ongoing first steps of development of an innovative centrifugal compressor stage designed for use in turboprop aircraft engines. The so-called tandem impeller blading concept shall be compared to the conventional blading design by means of numerical simulation and optimized to achieve the best possible parameters. In this paper, validation of a conventional stage computational model using experimental data is described. This paper presents the ongoing first steps of development of an innovative centrifugal compressor stage designed for use in turboprop aircraft engines. The so-called tandem impeller blading concept shall be compared to the conventional blading design by means of numerical simulation and optimized to achieve the best possible parameters. In this paper, validation of a conventional stage computational model using experimental data is described.
dcterms:title
Development of a Novel Centrifugal Compressor Stage for Aircraft Engines Development of a Novel Centrifugal Compressor Stage for Aircraft Engines
skos:prefLabel
Development of a Novel Centrifugal Compressor Stage for Aircraft Engines Development of a Novel Centrifugal Compressor Stage for Aircraft Engines
skos:notation
RIV/68407700:21260/14:00220451!RIV15-MSM-21260___
n3:aktivita
n19:S n19:I
n3:aktivity
I, S
n3:dodaniDat
n7:2015
n3:domaciTvurceVysledku
n15:5514495
n3:druhVysledku
n6:D
n3:duvernostUdaju
n16:S
n3:entitaPredkladatele
n13:predkladatel
n3:idSjednocenehoVysledku
10957
n3:idVysledku
RIV/68407700:21260/14:00220451
n3:jazykVysledku
n4:eng
n3:klicovaSlova
centrifugal compressor; turboprop engine. impeller; vaned diffuser; secondary flow; CFD
n3:klicoveSlovo
n5:secondary%20flow n5:CFD n5:vaned%20diffuser n5:turboprop%20engine.%20impeller n5:centrifugal%20compressor
n3:kontrolniKodProRIV
[F19A5C96CC3E]
n3:mistoKonaniAkce
Vyšší Brod - Herbertov
n3:mistoVydani
Brno
n3:nazevZdroje
New Trends in Civil Aviation 2014
n3:obor
n12:JU
n3:pocetDomacichTvurcuVysledku
1
n3:pocetTvurcuVysledku
2
n3:rokUplatneniVysledku
n7:2014
n3:tvurceVysledku
Hanus, Daniel Hlaváček, David
n3:typAkce
n8:EUR
n3:zahajeniAkce
2014-05-18+02:00
s:numberOfPages
7
n10:hasPublisher
Akademické nakladatelství CERM
n14:isbn
978-80-7204-891-5
n20:organizacniJednotka
21260