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dc.contributor.authorCHERDIEU, Patrick
dc.contributor.authorDUPONT, Patrick
dc.contributor.authorBAYEUL-LAINE, Annie-Claude
dc.contributor.authorBOIS, Gérard
dc.contributor.author
 hal.structure.identifier
DAZIN, Antoine
1252 Laboratoire de Mécanique de Lille - FRE 3723 [LML]
dc.date.accessioned2013
dc.date.available2013
dc.date.issued2013
dc.date.submitted2013
dc.identifier.urihttp://hdl.handle.net/10985/7601
dc.description.abstractAmong several different measurement techniques that have been already performed and presented in a radial impeller pump model including PIV, a directional pressure probe has been used to obtain mean velocity field and stagnation pressure between impeller outlet and the inlet vaned diffuser sections. These measurements are supposed to get more information not only about global pump head coefficient including vaned diffuser ones but also about impeller performances itself. Pressure probe information is affected by rotor-stator interactions and impeller rotation, and this paper presents a way to explain and correct pressure probe indications in order to achieve a better evaluation of overall impeller mean performances. The use of unsteady RANS calculation results is found to be a useful way to perform better data reduction analysis for this purpose
dc.language.isoen
dc.publisher6 th international conference on pimps and fans with compressors and wind turbines
dc.rightsPre-print
dc.subjectpump
dc.subjectdiffuser
dc.subjectcalculation
dc.subjectpIV measurements
dc.titleData reduction problems using a 3 holes directional pressure probe to investigate mean flow characteristics in the vaneless gap between impeller and diffuser radial pump
dc.identifier.doi10.1088/1757-899X/52/2/022018
dc.typdocCommunication avec acte
dc.localisationCentre de Lille
dc.subject.halSciences de l'ingénieur: Mécanique: Mécanique des fluides
ensam.audienceInternationale
ensam.conference.title6th ICPF conference
ensam.conference.date2013-09-19
ensam.countryChina
ensam.title.proceeding6 th ICPF conference
ensam.page6 pages
hal.identifierhal-00915099
hal.version1
hal.statusaccept


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