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Statements

Subject Item
n2:RIV%2F61388998%3A_____%2F10%3A00346319%21RIV11-MSM-61388998
rdf:type
skos:Concept n19:Vysledek
dcterms:description
This paper presents the experimental results of aerodynamic research performed on a blade cascade representing the midsection of 1220 mm long rotor blades of the last stage of a large output steam turbine. The operational regime of the blade cascade is characterized by supersonic exit velocity. Isentropic exit Mach number M2is = 1.323. The experimental data analysis concerns pneumatic measurements to calculate the total pressure and the kinetic energy loss coefficients, and to evaluate them mainly with respect to the aperiodicity of the flow field. The flow structure is also studied on the basis of results obtained by means of optical methods, such as schlieren and interferometric methods. This paper presents the experimental results of aerodynamic research performed on a blade cascade representing the midsection of 1220 mm long rotor blades of the last stage of a large output steam turbine. The operational regime of the blade cascade is characterized by supersonic exit velocity. Isentropic exit Mach number M2is = 1.323. The experimental data analysis concerns pneumatic measurements to calculate the total pressure and the kinetic energy loss coefficients, and to evaluate them mainly with respect to the aperiodicity of the flow field. The flow structure is also studied on the basis of results obtained by means of optical methods, such as schlieren and interferometric methods.
dcterms:title
LOSS COEFFICIENT DEPENDENCE OF TURBINE BLADE CASCADE LOSS COEFFICIENT DEPENDENCE OF TURBINE BLADE CASCADE
skos:prefLabel
LOSS COEFFICIENT DEPENDENCE OF TURBINE BLADE CASCADE LOSS COEFFICIENT DEPENDENCE OF TURBINE BLADE CASCADE
skos:notation
RIV/61388998:_____/10:00346319!RIV11-MSM-61388998
n4:aktivita
n17:P n17:Z
n4:aktivity
P(1M06031), P(1M06059), P(GA101/08/1112), P(IAA200760801), Z(AV0Z20760514)
n4:dodaniDat
n7:2011
n4:domaciTvurceVysledku
n6:5890780 n6:2157810
n4:druhVysledku
n10:D
n4:duvernostUdaju
n18:S
n4:entitaPredkladatele
n12:predkladatel
n4:idSjednocenehoVysledku
268933
n4:idVysledku
RIV/61388998:_____/10:00346319
n4:jazykVysledku
n9:eng
n4:klicovaSlova
loss coefficient; turbine cascade; pneumatic measurement
n4:klicoveSlovo
n8:pneumatic%20measurement n8:loss%20coefficient n8:turbine%20cascade
n4:kontrolniKodProRIV
[8814A8AC29B4]
n4:mistoKonaniAkce
Glasgow
n4:mistoVydani
Glasgow
n4:nazevZdroje
Proceedings of ASME Turbo Expo 2010: Power for Land, Sea and Air GT2010
n4:obor
n13:BK
n4:pocetDomacichTvurcuVysledku
2
n4:pocetTvurcuVysledku
5
n4:projekt
n15:1M06059 n15:1M06031 n15:GA101%2F08%2F1112 n15:IAA200760801
n4:rokUplatneniVysledku
n7:2010
n4:tvurceVysledku
Synáč, J. Luxa, Martin Matějka, M. Šimurda, David Šafařík, P.
n4:typAkce
n21:WRD
n4:zahajeniAkce
2010-06-14+02:00
n4:zamer
n5:AV0Z20760514
s:numberOfPages
9
n16:hasPublisher
ASME
n14:isbn
978-0-7918-3872-3