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1.Anne-Lise FIQUETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2024).
UHBR open-test case fan ECL5/CATANA: non-linear analysis of non-synchronous blade vibration at part-speed conditions
J. Turbomach. 146, 071003 (8 pages). doi:10.1115/1.4064841 doi.ico openalex-16x16.png
2.Cédric BABIN, Xavier OTTAVYorcid_16x16.png, Fabrizio FONTANETO (2023).
Leakage flow impact on shrouded stator cavity flow topology and associated high-speed axial compressor stage performance
J. Turbomach. 145, 051016 (13 pages). doi:10.1115/1.4056698 doi.ico openalex-16x16.png
3.Christoph BRANDSTETTERorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Benoît PAOLETTI, Sina STAPELFELDTorcid_16x16.png (2022).
Interpretation of stall precursor signatures
J. Turbomach. 143, 121011 (13 pages). doi:10.1115/1.4051709 doi.ico openalex-16x16.png
4.Ivo DAWKINS, James TAYLOR, Xavier OTTAVYorcid_16x16.png, Rob MILLER (2022).
The unsteady topology of corner separations
J. Turbomach. 144, 111001 (14 pages). doi:10.1115/1.4054676 doi.ico openalex-16x16.png
5.Jérôme BOUDETorcid_16x16.png, Emmanuel LÉVÊQUEorcid_16x16.png, Hatem TOUIL (2022).
Unsteady lattice Boltzmann simulations of corner separation in a compressor cascade
J. Turbomach. 144, 011010 (12 pages). doi:10.1115/1.4052017 doi.ico hal.ico openalex-16x16.png
6.Anne-Lise FIQUETorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png, Nicolas BUFFAZ, Agathe VERCOUTTER (2021).
Acoustic resonance in an axial multistage compressor leading to non-synchronous blade vibration
J. Turbomach. 143, 091014 (10 pages). doi:10.1115/1.4050626 doi.ico hal.ico openalex-16x16.png
7.Sina STAPELFELDTorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2021).
Suppression of nonsynchronous vibration through intentional aerodynamic and structural mistuning
J. Turbomach. 144, 021008 (8 pages). doi:10.1115/1.4052233 doi.ico openalex-16x16.png
8.Martin RODRIGUES, Laurent SOULAT, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2021).
Aerodynamic investigation of a composite low-speed fan for UHBR application
J. Turbomach. 143, 101004 (12 pages). doi:10.1115/1.4050671 doi.ico openalex-16x16.png
9.Thomas BONTEMPS, Stéphane AUBERTorcid_16x16.png, Maxime DE PRET (2021).
Prediction of the acoustic reflection in a realistic aeroengine intake with three numerical methods to analyze fan flutter
J. Turbomach. 143, 101016 (11 pages). doi:10.1115/1.4051113 doi.ico hal.ico openalex-16x16.png
10.Nicolas POUJOL, Isabelle TRÉBINJAC, Pierre DUQUESNEorcid_16x16.png (2021).
Effects of inlet guide vanes on the performance and stability of an aeronautical centrifugal compressor
J. Turbomach. 143, 101010 (9 pages). doi:10.1115/1.4050944 doi.ico hal.ico openalex-16x16.png
11.Christoph BRANDSTETTERorcid_16x16.png, Valdo PAGÈS, Pierre DUQUESNEorcid_16x16.png, Benoît PAOLETTI, Stéphane AUBERTorcid_16x16.png, Xavier OTTAVYorcid_16x16.png (2019).
Project PHARE-2 – a high-speed UHBR fan test facility for a new open-test-case
J. Turbomach. 141, 101004 (9 pages). doi:10.1115/1.4043883 doi.ico hal.ico openalex-16x16.png
12.Christoph BRANDSTETTERorcid_16x16.png, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png (2019).
Compressible modal instability onset in an aerodynamically mistuned transonic fan
J. Turbomach. 141, 031004 (11 pages). doi:10.1115/1.4042310 doi.ico hal.ico openalex-16x16.png
13.Anne-Lise FIQUETorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Mickaël PHILIT (2019).
Non-synchronous aeroacoustic interaction in an axial multi-stage compressor
J. Turbomach. 141, 101013 (8 pages). doi:10.1115/1.4044675 doi.ico openalex-16x16.png
14.Quentin RENDU, Yannick ROZENBERG, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND (2017).
Influence of acoustic blockage on flutter instability in a transonic nozzle
J. Turbomach. 140, 021004 (10 pages). doi:10.1115/1.4038279 doi.ico hal.ico openalex-16x16.png
15.Yannick BOUSQUET, Nicolas BINDER, Guillaume DUFOUR, Xavier CARBONNEAUorcid_16x16.png, Mathieu ROUMEAS, Isabelle TRÉBINJAC (2016).
Numerical simulation of stall inception mechanisms in centrifugal compressor with vaned diffuser
J. Turbomach. 138, 071007 (9 pages). doi:10.1115/1.4032457 doi.ico hal.ico openalex-16x16.png
16.Emmanuel BENICHOU, Isabelle TRÉBINJAC (2016).
Comparison of steady and unsteady flows in a transonic radial vaned diffuser
J. Turbomach. 138, 121002 (10 pages). doi:10.1115/1.4033481 doi.ico hal.ico openalex-16x16.png
17.Yannick BOUSQUET, Nicolas BINDER, Guillaume DUFOUR, Xavier CARBONNEAUorcid_16x16.png, Isabelle TRÉBINJAC, Mathieu ROUMEAS (2016).
Numerical investigation of Kelvin-Helmholtz instability in a centrifugal compressor operating near stall
J. Turbomach. 138, 071007 (9 pages). doi:10.1115/1.4032457 doi.ico hal.ico openalex-16x16.png
18.Jérôme BOUDETorcid_16x16.png, Adrien CAHUZAC, Philip KAUSCHE, Marc C. JACOBorcid_16x16.png (2015).
Zonal large-eddy simulation of a fan tip-clearance flow, with evidence of vortex wandering
J. Turbomach. 137, 061001 (9 pages). doi:10.1115/1.4028668 doi.ico hal.ico openalex-16x16.png
19.Aurélien MARSAN, Isabelle TRÉBINJAC, Sylvain COSTE, Gilles LEROY (2015).
Influence of unsteadiness on the control of a hub-corner separation within a radial vaned diffuser
J. Turbomach. 137, 021008 (12 pages). doi:10.1115/1.4028244 doi.ico hal.ico openalex-16x16.png
20.Flore CREVEL, Nicolas GOURDAINorcid_16x16.png, Xavier OTTAVYorcid_16x16.png (2014).
Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on its test rig - Part II: deep surge
J. Turbomach. 2014, 101004 (15 pages). doi:10.1115/1.4027968 doi.ico hal.ico openalex-16x16.png
21.Flore CREVEL, Nicolas GOURDAINorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2014).
Numerical simulation of aerodynamic instabilities in a multistage high-speed high-pressure compressor on its test-rig - Part I : rotating stall
J. Turbomach. 136, 101003 (14 pages). doi:10.1115/1.4027967 doi.ico hal.ico openalex-16x16.png
22.Pierre GOUGEON, Ghislaine NGO BOUM (2014).
Aerodynamic interactions between a high-pressure turbine and the first low-pressure stator
J. Turbomach. 136, 071010 (11 pages). doi:10.1115/1.4025955 doi.ico hal.ico openalex-16x16.png
23.William RIÉRA, Lionel CASTILLON, Julien MARTY, Francis LEBOEUF (2013).
Inlet condition effects on the tip clearance flow with zonal detached eddy simulation
J. Turbomach. 136, 041018 (10 pages). doi:10.1115/1.4025216 doi.ico hal.ico openalex-16x16.png
24.Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png (2013).
Experimental study of surge precursors in a high-speed multistage compressor
J. Turbomach. 135, 061018 (9 pages). doi:10.1115/1.4023462 doi.ico hal.ico openalex-16x16.png
25.Nicolas GOURDAINorcid_16x16.png, Fabien WLASSOW, Xavier OTTAVYorcid_16x16.png (2012).
Effect of tip clearance dimensions and control of unsteady flows in a multi-stage high-pressure compressor
J. Turbomach. 134, 051005 (13 pages). doi:10.1115/1.4003815 doi.ico openalex-16x16.png
26.Nicolas GOURDAINorcid_16x16.png, Francis LEBOEUF (2009).
Unsteady simulation of an axial compressor stage with casing and blade passive treatments
J. Turbomach. 131, 021013 (12 pages). doi:10.1115/1.2988156 doi.ico openalex-16x16.png
27.Isabelle TRÉBINJAC, Pascale KULISAorcid_16x16.png, Nicolas BULOT, Nicolas ROCHUON (2009).
Effect of unsteadiness on the performance of a transonic centrifugal compressor stage
J. Turbomach. 131, 041011 (9 pages). doi:10.1115/1.3070575 doi.ico openalex-16x16.png
28.Xavier OTTAVYorcid_16x16.png, Stéphane VILMIN, Howard HODSON, Simon GALLIMORE (2004).
The effects of wake-passing unsteadiness over a highly loaded compressor-like flat plate.
J. Turbomach. 126, 24–34. doi:10.1115/1.1643384 doi.ico hal.ico openalex-16x16.png
29.Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC, André VOUILLARMET (2001).
Analysis of the inter-row flow field within a transonic axial compressor : Part 2 - Unsteady flow analysis.
J. Turbomach. 123, 57–63. doi:10.1115/1.1328086 doi.ico hal.ico openalex-16x16.png
30.Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC, André VOUILLARMET (2001).
Analysis of the inter-row flow field within a transonic axial compressor : Part 1 - Experimental investigation.
J. Turbomach. 123, 49–56. doi:10.1115/1.1328085 doi.ico hal.ico openalex-16x16.png
31.G. PERRIN, Francis LEBOEUF (1995).
Investigation of troughflow hypothesis in a turbine cascade using a three-dimensional Navier-Stokes computation.
J. Turbomach. 117, 126–132.
32.Pascale KULISAorcid_16x16.png, Francis LEBOEUF, G. PERRIN (1992).
Computation of a wall boundary layer with discrete jet injections.
J. Turbomach. 114.
33.François BARIO, L. BARRAL, G. BOIS (1989).
Air test flow analysis of the hydrogen pump of Vulcain rocket engine.
J. Turbomach. 113, 654–659.
 
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