Laboratoire de Mécanique des Fluides et d'Acoustique - UMR 5509

LMFA - UMR 5509
Laboratoire de Mécanique des Fluides et d’Acoustique
Lyon
France


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Accueil > Pages perso > Trebinjac Isabelle > Recherche > Publications

Publications

2016

Bousquet Y, Binder N, Dufour G, Carbonneau X, Trébinjac I, Roumeas M. Numerical investigation of Kelvin-Helmholtz instability in a centrifugal compressor operating near stall. J. Turbomach.. 2016;138:071007.

2015

Benichou E, Trébinjac I. Analyse numérique d'un décollement alterné dans un diffuseur radial transsonique. Courbevoie: Association Française de Mécanique; 2015. CFM 2015 : Congrès Français de Mécanique, Lyon, France, 24-29/08/2015.
Benichou E, Trébinjac I. Application of an analytical method to locate a mixing Ppane in a supersonic compressor. J. Power Energy Eng.. 2015;9:91–101.
Benichou E, Trébinjac I. Steady/unsteady diffuser flow in a transonic centrifugal compressor. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2015. 11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Madrid, Spain, 23-27/0.
Bousquet Y, Carbonneau X, Trébinjac I, Binder N, Dufour G. Numerical investigation of kelvin-helmholtz instability in a centrifugal compressor operating near stall. New York, USA: Asme; 2015:113665. ASME Turbo Expo 2015, Montreal, Canada, 15-19/06/2015.
Marsan A, Trébinjac I, Coste S, Leroy G. Influence of unsteadiness on the control of a hub-corner separation within a radial vaned diffuser. J. Turbomach.. 2015;137:021008.
Tang E, Trébinjac I, Ngo Boum G, Philit M, Leroy G. Influence d'une injection d'air secondaire par une fente au carter dans l'espace stator-rotor sur l'aérodynamique d'une turbine haute pression. Courbevoie: Association Française de Mécanique; 2015. CFM 2015 : Congrès Français de Mécanique, Lyon, France, 24-29/08/2015.
Trébinjac I, Buffaz N, Benichou E. Full-Annulus Simulation of the Surge Inception in a Transonic Centrifugal Compressor. J. Therm. Sci.. 2015;24:442–451.

2014

Benichou E, Trébinjac I. Application of an analytical method to locate a mixing plane in a supersonic compressor. New York, USA: Asme; 2014:V02bt39a002. ASME Turbo Expo 2014, Düsseldorf, Germany, 16-20/06/2014.
Boudet J, Gao F, De Crécy F, et al. Research frontiers for compressors in aero-engines [abstract].; 2014. 11th World Congress on Computational Mechanics (WCCM XI), Barcelona, Spain, 20-25/07/2014.
Bousquet Y, Carbonneau X, Dufour G, Binder N, Trébinjac I. Analysis of the unsteady flow field in a centrifugal compressor from peak efficiency to near stall with full-annulus simulations. Int. J. Rot. Machin.. 2014;2014:729629.
Bousquet Y, Carbonneau X, Trébinjac I, Dufour G, Roumeas M. Description of the unsteady flow pattern from peak efficiency to near surge in a subsonic centrifugal compressor stage. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2014:917–927. 10th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Lappeenranta, Finland,.
Buffaz N, Trébinjac I. Aerodynamic instabilities in transonic centrifugal compressor. Mech. Ind.. 2014;15:191–196.
Marsan A, Trébinjac I, Coste S, Leroy G. Influence of unsteadiness on the control of a hub-corner separation within a radial vaned diffuser. New York, USA: Asme; 2014:Gt2014–26985. ASME Turbo Expo 2014, Düsseldorf, Germany, 16-20/06/2014.
Marsan A, Trébinjac I, Coste S, Leroy G. Temporal behavior of a boundary layer separation within a radial vaned diffuser. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2014:983–995. 10th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Lappeenranta, Finland,.

2013

Marsan A, Trébinjac I, Coste S, Leroy G. Temporal behaviour of a corner separation in a radial vaned diffuser of a centrifugal compressor operating near surge. J. Therm. Sci.. 2013;22:555–564.

2012

Buffaz N, Trébinjac I. Detailed analysis of the flow in the inducer of a transonic centrifugal compressor. J. Therm. Sci.. 2012;21:1–12.
Legras G, Trébinjac I, Gourdain N, Ottavy X, Castillon L. A Novel approach to evaluate the benefits of casing treatment in axial compressors. Int. J. Rot. Machin.. 2012;2012:975407.
Marsan A, Trébinjac I, Coste S, Leroy G. Study and control of a radial vaned diffuser stall. Int. J. Rot. Machin.. 2012;2012:549048.

2011

Buffaz N, Trébinjac I. Detailed analysis of the flow in the inducer of a transonic centrifugal compressor. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2011. 10th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows,.
Legras G, Castillon L, Trébinjac I, Gourdain N. Flow mechanisms induced by non-axisymetric casing treatment in a transonic axial compressor. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2011:Isaif10–158. 10th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows,.
Legras G, Gourdain N, Trébinjac I. Extended methodology for analysing the flow mechanisms induced by casing treatment in compressor. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, 21-25/03/2011.
Legras G, Gourdain N, Trébinjac I, Ottavy X. Analysis of unsteadiness on casing treatment mechanisms in an axial compressor. New York, USA: Asme; 2011. ASME Turbo Expo 2011, Vancouver, Canada, 06-10/06/2011.
Trébinjac I, Bulot N, Buffaz N. Analysis of the flow in a transonic centrifugal compressor stage from choke to surge. Proc. IMechE Part A, J. Power Energy. 2011;225:919–929.
Trébinjac I, Bulot N, Buffaz N. Analysis of the flow in a transonic centrifugal compressor stage from choke to surge. Rhode-St-Genèse - Belgium: Von Karman Institute for Fluid Dynamics; 2011. 9th European Conference on Turbomachinery, Istanbul, Turkey, 21-25/03/2011.
Trébinjac I, Bulot N, Ottavy X, Buffaz N. Surge inception in a transonic centrifugal compressor stage. New York, USA: Asme; 2011. ASME Turbo Expo 2011, Vancouver, Canada, 06-10/06/2011.

2010

Buffaz N, Trébinjac I. Tip clearance effect on the flow field within a high-pressure centrifugal compressor. Ny, Usa: Curran Associates; 2010:1–9. 13th International Symposium on Transport Phenomena and Dynamics of Rotating Machinery, Honolulu, Ha.
Bulot N, Ottavy X, Trébinjac I. Unsteady pressure measurements in a high-speed centrifugal compressor. J. Therm. Sci.. 2010;19:1–8.
Leboeuf F, Trébinjac I, Ottavy X, Gourdain N. Aerodynamic studies in high-speed compressors dedicated to aeronautical applications.; 2010. 27th Congress of the International Council of the Aeronautical Sciences, Nice, France, 19-24/09/2010.
Legras G, Gourdain N, Trébinjac I. Numerical analysis of the tip leakage flow field in a transonic axial compressor with circumferential casing treatment. J. Therm. Sci.. 2010;19:198–205.

2009

Bulot N, Trébinjac I. Effect of the unsteadiness on the diffuser flow in a transonic centrifugal compressor stage. Int. J. Rot. Machin.. 2009;2009:932593.
Bulot N, Ottavy X, Trébinjac I. Unsteady pressure measurements in a high-speed centrifugal compressor.; 2009:Isaif9–066. 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, .
Bulot N, Trébinjac I, Ottavy X, et al. Experimental and numerical investigation of the flow field in a high-pressure centrifugal compressor impeller near surge. Proc. IMechE Part A, J. Power Energy. 2009;223:657–666.
Bulot N, Trébinjac I, Ottavy X, et al. Experimental and numerical investigation of the flow field in a high-pressure centrifugal compressor impeller near surge.; 2009:447–458. 8th European Turbomachinery Conference, Graz, Austria, 23-27/03/2009.
Ottavy X, Goguey S, Berthiau J, Trébinjac I. Doppler global velocimeter – development and validation with measurements in a round free jet. J. Therm. Sci.. 2009;1:74–84.
Trébinjac I, Kulisa P, Bulot N, Rochuon N. Effect of unsteadiness on the performance of a transonic centrifugal compressor stage. J. Turbomach.. 2009;131:041011.
Trébinjac I, Ottavy X, Rochuon N, Bulot N. On the validity of steady calculations with shock-blade row interaction in compressors.; 2009:Isaif9–062. 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, .

2008

Boudet J, Trébinjac I, Vouillarmet A, Echampard D. Une Nouvelle Pédagogie pour des Travaux Pratiques en Mécanique des Fluides.; 2008:87–94. Journées AUM / AFM 2008, Mulhouse, France, 27-29/08/2008.
Bulot N, Trébinjac I. Effect of the unsteadiness on the diffuser flow in a transonic centrifugal compressor stage.; 2008. 12th ISROMAC, Honolulu, United States, 17-22/02/2008.
Rochuon N, Trébinjac I, Kulisa P, Billonnet G. Assessment of jet-wake flow structures induced by three-dimensional hub wall contouring. Ireme. 2008;2:113–121.
Trébinjac I, Kulisa P, Bulot N, Rochuon N. Effect of the unsteadiness on the performance of a transonic centrifugal compressor stage. New York, USA: Asme; 2008:Gt 2008–50260. ASME Turbo Expo 2008: Power for Land, Sea and Air (TE08), Berlin, Germany, 09-13/06/2008.

2007

Bulot N, Trébinjac I. Impeller-diffuser interaction: analysis of the unsteady flow structures based on their direction of propagation. J. Therm. Sci.. 2007;16:193–202.
Bulot N, Trébinjac I. Impeller-diffuser interaction: analysis of the unsteady flow structures based on their direction of propagation.; 2007:Isaif8–00136. 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, .
Rochuon N, Trébinjac I, Kulisa P, Billonnet G. Using a 3D hub to avoid the jet-wake flow structure.; 2007. 7th European Conference on Turbomachinery, Athens, Greece, 05-09/03/2007.

2006

Trébinjac I, Rochuon N, Billonnet G. An extraction of the dominant rotor-stator interaction modes by the use of Proper Orthogonal Decomposition (POD). J. Therm. Sci.. 2006;15:109–114.

2005

Rochuon N, Trébinjac I. Proper Orthogonal Decomposition (POD) – Application to rotorstator interaction analysis. Ecole Nationale Supérieure d'Arts et Métiers; 2005:Paper 033_01/63. 6th European Conference on Turbomachinery, Lille, France, 07-11/03/2005.
Rochuon N, Trébinjac I, Billonnet G. An extraction of the dominant rotor-stator interaction modes by the use of Proper Orthogonal Decomposition (POD).; 2005. 7th ISAIF, Tokyo, Japan, 11-15/09/2005.
Trébinjac I, Charbonnier D, Leboeuf F. Unsteady rotor-stator interaction in high speed compressor and turbine stages. J. Therm. Sci.. 2005;14:289–297.

2003

Ottavy X, Trébinjac I, Vouillarmet A, Arnaud D. Laser measurements in high speed compressors for rotor-stator interaction analysis. Meas. Sci. Technol.. 2003;12:310–317.
Trébinjac I. Méthodologie d'étude des écoulements tridimensionnels et instationnaires dans les turbomachines à haute vitesse [Ph.D. thesis]. École centrale de Lyon; 2003.

2002

Trébinjac I, Vixege C. Experimental analysis of the rotor stator interaction within a high pressure centrifugal compressor. J. Therm. Sci.. 2002:1–9.

2001

Ottavy X, Trébinjac I, Vouillarmet A. Analysis of the inter-row flow field within a transonic axial compressor : Part 1 – Experimental investigation. J. Turbomach.. 2001;123:49–56.
Ottavy X, Trébinjac I, Vouillarmet A. Analysis of the inter-row flow field within a transonic axial compressor : Part 2 – Unsteady flow analysis. J. Turbomach.. 2001;123:57–63.

2000

Arnaud D, Ottavy X, Trébinjac I. Mesures par anémométrie laser L2F-2D et 3D en turbomachines : Traitement des distorsions optiques créées par des hublots courbes [abstract].; 2000. 7ème Congrès Francophone de Vélocimétrie Laser, Marseille, France, 19-22/09/2000.

1999

Ottavy X, Trébinjac I, Vouillarmet A. L2F anemometry measurements of the inter-row flow field within a transonic axial compressor proovided with curved windows. Meas. Sci. Technol.. 1999;8:166–175.

1998

Ottavy X, Trébinjac I, Vouillarmet A. Treatment of L2F anemometer measurement volume distorsions created by curved windows for turbomachinery application. Meas. Sci. Technol.. 1998;9:1511–1521.

1997

Trébinjac I, Claudin I. Results and analysis of a L2F flow field investigation within a high-speed high- pressure centrifugal compressor. J. Therm. Sci. VL -. 1997.

1996

Bois G, Leboeuf F, Trébinjac I, Vouillarmet A. Ecoulements tridimensionnels dans les turbomachines transsoniques et supersoniques. Int. J. Numer. Methods Heat Fluid Flow. 1996:117–130.

1995

Bois G, Leboeuf F, Trébinjac I, Vouillarmet A. Ecoulements tridimensionnels dans les turbomachines transsoniques et supersoniques. Revue Française de Mécanique. 1995;1996-2:117–130.