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Statements

Subject Item
n2:RIV%2F61388998%3A_____%2F09%3A00329710%21RIV10-AV0-61388998
rdf:type
n9:Vysledek skos:Concept
dcterms:description
The paper describes a role of experimental aerodynamic research oriented to the support of the design and computauion of turbomachines. The research techniques are briefly introduced. They are namely optical measurements of flow fields and pneumatic measurements by means of traversing. Results of the high-speed aerodynamic modelling of the flow past a blade cascade cascade representing a section in the balding of the last stage of a large output steam turbine are presented. The paper describes a role of experimental aerodynamic research oriented to the support of the design and computauion of turbomachines. The research techniques are briefly introduced. They are namely optical measurements of flow fields and pneumatic measurements by means of traversing. Results of the high-speed aerodynamic modelling of the flow past a blade cascade cascade representing a section in the balding of the last stage of a large output steam turbine are presented.
dcterms:title
Experimental AErodynamic research as a Support of the Design and Computation of Turbomachines Experimental AErodynamic research as a Support of the Design and Computation of Turbomachines
skos:prefLabel
Experimental AErodynamic research as a Support of the Design and Computation of Turbomachines Experimental AErodynamic research as a Support of the Design and Computation of Turbomachines
skos:notation
RIV/61388998:_____/09:00329710!RIV10-AV0-61388998
n4:aktivita
n16:P n16:Z
n4:aktivity
P(GA101/08/0623), P(IAA200760801), Z(AV0Z20760514)
n4:dodaniDat
n6:2010
n4:domaciTvurceVysledku
n13:8412472 n13:2157810 n13:5890780
n4:druhVysledku
n15:D
n4:duvernostUdaju
n19:S
n4:entitaPredkladatele
n21:predkladatel
n4:idSjednocenehoVysledku
314180
n4:idVysledku
RIV/61388998:_____/09:00329710
n4:jazykVysledku
n10:eng
n4:klicovaSlova
high speed aerodynamics; blade cascade; transonic flow; supersonic flow
n4:klicoveSlovo
n7:high%20speed%20aerodynamics n7:transonic%20flow n7:supersonic%20flow n7:blade%20cascade
n4:kontrolniKodProRIV
[432DC7CF55BF]
n4:mistoKonaniAkce
Praha
n4:mistoVydani
Praha
n4:nazevZdroje
Současné trendy při návrhu a výpočtu turbostrojů
n4:obor
n12:BK
n4:pocetDomacichTvurcuVysledku
3
n4:pocetTvurcuVysledku
3
n4:projekt
n5:IAA200760801 n5:GA101%2F08%2F0623
n4:rokUplatneniVysledku
n6:2009
n4:tvurceVysledku
Luxa, Martin Šafařík, Pavel Šimurda, David
n4:typAkce
n14:EUR
n4:zahajeniAkce
2009-06-02+02:00
n4:zamer
n17:AV0Z20760514
s:numberOfPages
8
n11:hasPublisher
TechSoft Engineering s.r.o.
n20:isbn
978-80-254-4651-5