The impact of low solidity vaned diffusers (LSVDs) on rotating stall and performance was investigated in an industrial centrifugal stage initially designed with a vaneless diffuser. The activity was based on the coupled use of advanced measurement techniques and 3D fully-viscous computations. Experimental data at the impeller inlet was used as boundary conditions in 3D computations, in order to reproduce actual test working conditions. In previous studies the effectiveness of LSVDs for stall control was shown. In this work attention was focused on the effects of LSVDs on the performance curve. Three diffusers were designed and tested in order to achieve a stage performance curve close to the vaneless one or even better. The parameters changed are incidence at design point and blade deflection (blade exit angle compared with free vortex stream line at design point). The main results of this activity are presented and discussed.

A coupled experimental/numerical analysis for low solidity vaned diffusers performance optimization / P. BONCINELLI; G. FERRARA; L. FERRARI; L. BALDASSARRE. - STAMPA. - (2006), pp. 490-498. (Intervento presentato al convegno ISROMAC, The 11th of International Symposium on Transport Phenomena and Dynamics of Rotating Machinery tenutosi a Honolulu, Hawaii nel February 26-March 2, 2006).

A coupled experimental/numerical analysis for low solidity vaned diffusers performance optimization

FERRARA, GIOVANNI;FERRARI, LORENZO;
2006

Abstract

The impact of low solidity vaned diffusers (LSVDs) on rotating stall and performance was investigated in an industrial centrifugal stage initially designed with a vaneless diffuser. The activity was based on the coupled use of advanced measurement techniques and 3D fully-viscous computations. Experimental data at the impeller inlet was used as boundary conditions in 3D computations, in order to reproduce actual test working conditions. In previous studies the effectiveness of LSVDs for stall control was shown. In this work attention was focused on the effects of LSVDs on the performance curve. Three diffusers were designed and tested in order to achieve a stage performance curve close to the vaneless one or even better. The parameters changed are incidence at design point and blade deflection (blade exit angle compared with free vortex stream line at design point). The main results of this activity are presented and discussed.
2006
Proceedings of the 11th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, ISROMAC-11
ISROMAC, The 11th of International Symposium on Transport Phenomena and Dynamics of Rotating Machinery
Honolulu, Hawaii
February 26-March 2, 2006
P. BONCINELLI; G. FERRARA; L. FERRARI; L. BALDASSARRE
File in questo prodotto:
File Dimensione Formato  
ISROMAC-11_ferrara_giovanni_paper17_final.pdf

Accesso chiuso

Tipologia: Altro
Licenza: Tutti i diritti riservati
Dimensione 1.1 MB
Formato Adobe PDF
1.1 MB Adobe PDF   Richiedi una copia

I documenti in FLORE sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/318378
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus 0
  • ???jsp.display-item.citation.isi??? ND
social impact