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ASME Turbo Expo 2004: Power for Land, Sea, and Air | 2004

Aerodynamic Design and Test Result Analysis of a Three Stage Research Compressor

Armel Touyeras; Michel Villain

The present paper describes the aerodynamic design and the test result analysis of a three-stage research compressor designed by Snecma Moteurs and tested at Ecole Centrale de Lyon, France. Firstly, the CREATE compressor, representative of the median or rear stages of modern high-pressure compressors, is presented. Particular emphasis is put on the CFD process employed in its design, which was based largely on three-dimensional Navier-Stokes multistage simulations. A brief description of the stage-by-stage matching achieved on the compressor is also presented. Test results available from traversal probes and laser velocimetry are compared with CFD simulation for overall compressor performance, stage-by-stage matching, and secondary flow effects. Prediction of the design and off-design compressor performance with 3D multistage tools is discussed. Finally, the prospects of new developments concerning the CFD tools and the evolution of the experimental compressor are also mentioned.Copyright


Archive | 2009

Compressor casing with optimized cavities

Xavier Agneray; Jerome Jean Bert; Alexandre Franck Arnaud Chartoire; Armel Touyeras


Archive | 2010

TURBINE ENGINE COMPRESSOR HAVING AIR INJECTIONS

Michel Andre Bouru; Laurent Jablonski; Armel Touyeras


Archive | 2009

Carter de compresseur a cavites optimisees

Xavier Agneray; Jerome Jean Bert; Alexandre Franck Arnaud Chartoire; Armel Touyeras


Archive | 2006

Taking air away from the tips of the rotor wheels of a high pressure compressor in a turbojet

Armel Touyeras


Archive | 2009

Turbomachine compressor with an air injection system

Xavier Agneray; Alexandre Franck Arnaud Chartoire; Armel Touyeras; Julien Loucheux


Archive | 2015

Bleeding air from the tip of the rotating blades in a high pressure compressor of a turbine engine

Armel Touyeras


Archive | 2011

ENGINE COMPRESSOR, PARTICULARLY AIRCRAFT JET ENGINE COMPRESSOR, FITTED WITH AN AIR BLEED SYSTEM

Armel Touyeras


Archive | 2009

turbomachine compressor having air nozzles

Michel Andre Bouru; Laurent Jablonski; Armel Touyeras


Archive | 2009

Turbine engine compressor comprising an air injection system

Xavier Agneray; Alexandre Franck Arnaud Chartoire; Armel Touyeras; Julien Loucheux

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