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Statements

Subject Item
n2:RIV%2F49777513%3A23640%2F09%3A00502852%21RIV10-GA0-23640___
rdf:type
skos:Concept n15:Vysledek
dcterms:description
Aerodynamic performance of highly loaded low-speed axial-flow compressor stage AV1 was computed by means of commercial code Fluent 6.3.26. The computed data were compared with experimental results obtained in test stage with external diameter of 600 mm. At design condition one could observe reasonable agreement. The difference between theoretical and measured characteristics increased with the growing distance of stage working point from design point. This conclusion is supported by the comparison of experimental and computed rotor and stator blade elements performance at three typical working conditions. Aerodynamic performance of highly loaded low-speed axial-flow compressor stage AV1 was computed by means of commercial code Fluent 6.3.26. The computed data were compared with experimental results obtained in test stage with external diameter of 600 mm. At design condition one could observe reasonable agreement. The difference between theoretical and measured characteristics increased with the growing distance of stage working point from design point. This conclusion is supported by the comparison of experimental and computed rotor and stator blade elements performance at three typical working conditions. Aerodynamic performance of highly loaded low-speed axial-flow compressor stage AV1 was computed by means of commercial code Fluent 6.3.26. The computed data were compared with experimental results obtained in test stage with external diameter of 600 mm. At design condition one could observe reasonable agreement. The difference between theoretical and measured characteristics increased with the growing distance of stage working point from design point. This conclusion is supported by the comparison of experimental and computed rotor and stator blade elements performance at three typical working conditions.
dcterms:title
NUMERICAL INVESTIGATION of HIGHLY LOADED SINGLE-STAGE AXIAL-FLOW COMPRESSOR NUMERICAL INVESTIGATION of HIGHLY LOADED SINGLE-STAGE AXIAL-FLOW COMPRESSOR NUMERICAL INVESTIGATION of HIGHLY LOADED SINGLE-STAGE AXIAL-FLOW COMPRESSOR
skos:prefLabel
NUMERICAL INVESTIGATION of HIGHLY LOADED SINGLE-STAGE AXIAL-FLOW COMPRESSOR NUMERICAL INVESTIGATION of HIGHLY LOADED SINGLE-STAGE AXIAL-FLOW COMPRESSOR NUMERICAL INVESTIGATION of HIGHLY LOADED SINGLE-STAGE AXIAL-FLOW COMPRESSOR
skos:notation
RIV/49777513:23640/09:00502852!RIV10-GA0-23640___
n4:aktivita
n12:P
n4:aktivity
P(GA101/09/1959)
n4:dodaniDat
n14:2010
n4:domaciTvurceVysledku
n7:5496349 n7:9453318
n4:druhVysledku
n6:O
n4:duvernostUdaju
n17:S
n4:entitaPredkladatele
n16:predkladatel
n4:idSjednocenehoVysledku
330211
n4:idVysledku
RIV/49777513:23640/09:00502852
n4:jazykVysledku
n11:cze
n4:klicovaSlova
axial-flow compressor; comparison; aerodynamic characteristics
n4:klicoveSlovo
n13:axial-flow%20compressor n13:comparison n13:aerodynamic%20characteristics
n4:kontrolniKodProRIV
[C995A7D8BAD4]
n4:obor
n10:BK
n4:pocetDomacichTvurcuVysledku
2
n4:pocetTvurcuVysledku
2
n4:projekt
n9:GA101%2F09%2F1959
n4:rokUplatneniVysledku
n14:2009
n4:tvurceVysledku
Polanský, Jiří Dvořák, Dalibor
n8:organizacniJednotka
23640