The performance of an axial compressor with either shrouded or cantilevered stators has been analyzed. The two configurations have been compared both at design and near stall operating conditions, with the aid of CFD and experimental measurements. Results show that shrouded or cantilevered stators impact differently on the overall performance of the tested compressor. A higher stall margin occurs with the cantilevered build, while the work coefficient and the efficiency of the shrouded build at design conditions are higher. An overall comparison of the shrouded and cantilevered design concepts has been carried out, not only in aerodynamic but also in economic terms.

Complementary Use of CFD and Experimental Measurements to Assess the Impact of Shrouded and Cantilevered Stators in Axial Compressors / A. Arnone; P. Boncinelli; M. S. Campobasso; A. Mattheiss; U. Wenger. - ELETTRONICO. - 1: Aircraft Engine; Marine; Turbomachinery; Microturbines and Small Turbomachinery:(1999), pp. 1-11. (Intervento presentato al convegno ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition tenutosi a Indianapolis, Indiana, USA nel June 7-10) [10.1115/99-GT-208].

Complementary Use of CFD and Experimental Measurements to Assess the Impact of Shrouded and Cantilevered Stators in Axial Compressors

ARNONE, ANDREA;
1999

Abstract

The performance of an axial compressor with either shrouded or cantilevered stators has been analyzed. The two configurations have been compared both at design and near stall operating conditions, with the aid of CFD and experimental measurements. Results show that shrouded or cantilevered stators impact differently on the overall performance of the tested compressor. A higher stall margin occurs with the cantilevered build, while the work coefficient and the efficiency of the shrouded build at design conditions are higher. An overall comparison of the shrouded and cantilevered design concepts has been carried out, not only in aerodynamic but also in economic terms.
1999
Conference Proceedings
ASME 1999 International Gas Turbine and Aeroengine Congress and Exhibition
Indianapolis, Indiana, USA
June 7-10
A. Arnone; P. Boncinelli; M. S. Campobasso; A. Mattheiss; U. Wenger
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Utilizza questo identificatore per citare o creare un link a questa risorsa: https://hdl.handle.net/2158/356665
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