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articles
1.Christoph BRANDSTETTER, Valdo PAGÈS, Pierre DUQUESNE, Benoît PAOLETTI, Stéphane AUBERT, Xavier OTTAVYorcid_16x16.png (2019).
Project PHARE-2 – a High-Speed UHBR Fan Test Facility for a new Open-Test-Case
J. Turbomach. . doi:DOI: 10.1115/1.4043883 doi.ico clarivate_16x16.png
2.Christoph BRANDSTETTER, 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 clarivate_16x16.png
3.Zhiyuan LI, Juan DU, Xavier OTTAVYorcid_16x16.png, Hongwu ZHANG (2018).
Quantification and analysis of the irreversible flow loss in a linear compressor cascade
Entropy 20, 486 (16 pages). doi:10.3390/e20070486 doi.ico hal.ico clarivate_16x16.png
4.Johannes SCHREIBER, Benoît PAOLETTI, Xavier OTTAVYorcid_16x16.png (2017).
Observations on rotating instabilities and spike type stall inception in a high-speed multistage compressor
Int. J. Rot. Machin. 2017, 7035870 (11 pages). doi:10.1155/2017/7035870 doi.ico hal.ico clarivate_16x16.png
5.Gherardo ZAMBONINI, Xavier OTTAVYorcid_16x16.png, Jochen KRIEGSEIS (2017).
Corner separation dynamics in a linear compressor cascade
J. Fluids Eng. 139, 061101 (13 pages). doi:10.1115/1.4035876 doi.ico hal.ico clarivate_16x16.png
6.Feng GAO, Wei MA, Jinjing SUN, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Yangwei LIU, Lipeng LU, Liang SHAOorcid_16x16.png (2017).
Parameter study on numerical simulation of corner separation in LMFA-NACA65 linear compressor cascade
Chin. J. Aeronauti. 30, 15–30. doi:10.1016/j.cja.2016.09.015 doi.ico hal.ico clarivate_16x16.png
7.Hongwei MA, Wei WEI, Xavier OTTAVYorcid_16x16.png (2017).
Experimental investigation of flow field in a laboratory-scale compressor
Chin. J. Aeronauti. 30, 31–46. doi:10.1016/j.cja.2016.09.016 doi.ico hal.ico clarivate_16x16.png
8.Jinjing SUN, Xavier OTTAVYorcid_16x16.png (2016).
Control of corner separation by optimized slot configuration in a linear compressor cascade
Compressor Blower and Fan Technology 6 (10 pages). doi:10.16492/j.fjjs.2016.06.0056 doi.ico hal.ico clarivate_16x16.png
9.Lionel CASTILLON, Nicolas GOURDAIN, Xavier OTTAVYorcid_16x16.png (2015).
Multiple-frequency phase-lagged unsteady simulations of experimental axial compressor
J. Propul. Power 31, 444–455. doi:10.2514/1.B35247 doi.ico hal.ico clarivate_16x16.png
10.Feng GAO, Gherardo ZAMBONINI, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Liang SHAOorcid_16x16.png (2015).
Unsteady behavior of corner separation in a compressor cascade: Large eddy simulation and experimental study
Proc. IMechE Part A, J. Power Energy 229, 508–519. doi:10.1177/0957650915594314 doi.ico hal.ico clarivate_16x16.png
11.Feng GAO, Wei MA, Gherardo ZAMBONINI, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Liang SHAOorcid_16x16.png (2015).
Large-eddy simulation of 3-D corner separation in a linear compressor cascade
Phys. Fluids 27, 085105 (21 pages). doi:10.1063/1.4928246 doi.ico hal.ico clarivate_16x16.png
12.Flore CREVEL, Nicolas GOURDAIN, 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 clarivate_16x16.png
13.Wei MA, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Francis LEBOEUF (2013).
Effect of an adverse pressure gradient on the streamwise Reynolds stress profile maxima in a turbulent boundary layer
Acta Mech. Sin. 29 (4 pages). doi:10.1007/s10409-013-0033-2 doi.ico hal.ico clarivate_16x16.png
14.Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png (2013).
Study of the acoustic resonance occurring in a multistage high-speed axial compressor
Proc. IMechE Part A, J. Power Energy 227, 654–664. doi:10.1177/0957650913500493 doi.ico hal.ico clarivate_16x16.png
15.Mehmet MERSINLIGIL, Jean-François BROUCKAERT, Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png (2013).
On using fast response pressure sensors in aerodynamic probes to measure total temperature and entropy generation in turbomachinery blade rows
J. Eng. Gas Turbine Power 135, 101601 (10 pages). doi: 10.1115/1.4024999 doi.ico hal.ico clarivate_16x16.png
16.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 clarivate_16x16.png
17.Wei MA, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Francis LEBOEUF (2013).
Intermittent corner separation in a linear compressor cascade
Exp. Fluids 54, 1–17. doi:10.1007/s00348-013-1546-y doi.ico hal.ico clarivate_16x16.png
18.Xavier OTTAVYorcid_16x16.png, Nicolas COURTIADE, Nicolas GOURDAIN (2012).
Experimental and Computational Methods for Flow Investigation in High-Speed Multistage Compressor
J. Propul. Power 28, 1141–1155. doi:10.2514/1.60562 doi.ico clarivate_16x16.png
19.Guillaume LEGRAS, Isabelle TRÉBINJAC, Nicolas GOURDAIN, Xavier OTTAVYorcid_16x16.png, Lionel CASTILLON (2012).
A Novel approach to evaluate the benefits of casing treatment in axial compressors
Int. J. Rot. Machin. 2012, 975407 (19 pages). doi:10.1155/2012/975407 doi.ico clarivate_16x16.png
20.Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png, Nicolas GOURDAIN (2012).
Modal decomposition for the analysis of the rotor-stator interactions in multistage compressors
J. Therm. Sci. 21, 276–285. doi:10.1007/s11630-012-0545-2 doi.ico clarivate_16x16.png
21.Mehmet MERSINLIGIL, Jean-François BROUCKAERT, Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png (2012).
A high temperature high bandwidth fast response total pressure probe for measurements in a multistage axial compressor
J. Eng. Gas Turbine Power 134, 061601. doi:10.1115/1.4006061 doi.ico clarivate_16x16.png
22.Nicolas GOURDAIN, 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 clarivate_16x16.png
23.Wei MA, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Francis LEBOEUF, Feng GAO (2011).
Experimental study of corner stall in a linear compressor cascade
Chin. J. Aeronauti. 24, 235–242. doi:10.1016/S1000-9361(11)60028-9 doi.ico clarivate_16x16.png
24.Nicolas BULOT, Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC (2010).
Unsteady pressure measurements in a high-speed centrifugal compressor
J. Therm. Sci. 19, 1–8. doi:10.1007/s11630-010-0000-0 doi.ico clarivate_16x16.png
25.Xavier OTTAVYorcid_16x16.png, Sébastien GOGUEY, Juliane BERTHIAU, Isabelle TRÉBINJAC (2009).
Doppler global velocimeter - development and validation with measurements in a round free jet
J. Therm. Sci. 1, 74–84. doi:10.1007/s11630-009-0074-9 doi.ico hal.ico clarivate_16x16.png
26.Nicolas BULOT, Isabelle TRÉBINJAC, Xavier OTTAVYorcid_16x16.png, Pascale KULISA, G. HALTER, Benoît PAOLETTI, Patrick KRIKORIAN (2009).
Experimental and numerical investigation of the flow field in a high-pressure centrifugal compressor impeller near surge
Proc. IMechE Part A, J. Power Energy 223, 657–666. doi:10.1243/09576509JPE817 doi.ico clarivate_16x16.png
27.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 clarivate_16x16.png
28.Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC, André VOUILLARMET, D. ARNAUD (2003).
Laser measurements in high speed compressors for rotor-stator interaction analysis.
Meas. Sci. Technol. 12, 310–317. doi:10.1007/s11630-003-0036-6 doi.ico clarivate_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 clarivate_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 clarivate_16x16.png
31.Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC, André VOUILLARMET (1999).
L2F anemometry measurements of the inter-row flow field within a transonic axial compressor proovided with curved windows.
J. Therm. Sci. 8, 166–175. doi:10.1007/s11630-999-0003-y doi.ico hal.ico clarivate_16x16.png
32.Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC, André VOUILLARMET (1998).
Treatment of L2F anemometer measurement volume distorsions created by curved windows for turbomachinery applications
Meas. Sci. Technol. 9, 1511–1521. doi:10.1088/0957-0233/9/9/021 doi.ico hal.ico clarivate_16x16.png
 
thèses/hdr
1.Jinjing SUN (dir.: Xavier OTTAVY) (2018).
Investigation and control of three-dimensional separation/stall in compressors
Thèse École centrale de Lyon
2.Gherardo ZAMBONINI (dir.: Xavier OTTAVY) (2016).
Unsteady dynamics of corner separation in a linear compressor cascade
Thèse École centrale de Lyon hal.ico
3.Johannes SCHREIBER (dir.: Xavier OTTAVY) (2016).
Investigation of experimental and numerical methods, and analysis of stator clocking and instabilities in a high-speed multistage compressor
Thèse École centrale de Lyon hal.ico
4.Xavier OTTAVYorcid_16x16.png (2014).
Instationnarité et Instabilité dans les compresseurs aéronautiques
Habilitation École centrale de Lyon
5.Feng GAO (dir.: Liang SHAO, Jérôme BOUDET, Xavier OTTAVY, Lipeng LU) (2014).
Advanced numerical simulation of corner separation in a linear compressor cascade
Thèse École centrale de Lyon
6.Flore CREVEL (dir.: Nicolas GOURDAIN, Xavier OTTAVY) (2013).
Simulation numérique de l'écoulement en régime de pompage dans un compresseur axial multi-étage
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2364_fcrevel.pdf
7.Nicolas COURTIADE (dir.: Isabelle TRÉBINJAC, Xavier OTTAVY) (2012).
Etude de l'instationnarité et la rentrée en instabilité de l'écoulement dans le compresseur CREATE
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2315_ncourtiade.pdf
8.Xavier OTTAVYorcid_16x16.png (1999).
Mesures par Anémométrie laser dans un compresseur axial transsonique. Etudes des structures instationnaires périodiques.
Thèse École centrale de Lyon
 
conférences invitées
1.Jérôme BOUDETorcid_16x16.png, Feng GAO, Florence DE CRÉCY, Adrien CAHUZAC, Ghislaine NGO BOUM, Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC (2014).
Research frontiers for compressors in aero-engines
11th World Congress on Computational Mechanics (WCCM XI), Barcelona, Spain.
 
communications avec actes
1.Christoph BRANDSTETTER, Valdo PAGÈS, Pierre DUQUESNE, Benoît PAOLETTI, Stéphane AUBERT, Xavier OTTAVYorcid_16x16.png (2018).
Project PHARE-2 – a High-Speed UHBR Fan Test Facility for a new Open-Test-Case
15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines, Oxford, United Kingdom.
In: Proceedings of 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines, , .
2.Gherardo ZAMBONINI, Xavier OTTAVYorcid_16x16.png, Jochen KRIEGSEIS (2016).
Corner separation dynamics in a linear compressor cascade
ASME Turbo Expo 2016 : Turbomachinery Technical Conference and Exposition, Seoul, Korea, Republic of. doi:10.1115/GT2016-56454 doi.ico
In: Proceedings of the ASME Turbo Expo 2016, ASME, New York, USA. doi:10.1115/GT2016-56454 doi.ico
3.Wei MA, Feng GAO, Xavier OTTAVYorcid_16x16.png, Lipeng LU, A.J. WANG (2016).
Numerical investigation of intermittent corner separation in a linear compressor cascade
ASME Turbo Expo 2016 : Turbomachinery Technical Conference and Exposition, Seoul, Korea, Republic of. doi:10.1115/GT2016-57311 doi.ico
In: Proceedings of the ASME Turbo Expo 2016, ASME, New York, USA. doi:10.1115/GT2016-57311 doi.ico
4.Johannes SCHREIBER, Xavier OTTAVYorcid_16x16.png, Ghislaine NGO BOUM, Nicolas GOURDAIN (2016).
Influence of rotor tip flow field mis-prediction on rotating disturbance near surge in a high speed multistage compressor
ASME Turbo Expo 2016 : Turbomachinery Technical Conference and Exposition, Seoul, Korea, Republic of. doi:10.1115/GT2016-57372 doi.ico
In: Proceedings of the ASME Turbo Expo 2016, ASME, New York, USA. doi:10.1115/GT2016-57372 doi.ico
5.Feng GAO, Gherardo ZAMBONINI, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Liang SHAOorcid_16x16.png (2015).
Unsteady behavior of corner separation in a compressor cascade-LES and experimental study
11th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Madrid, Spain.
In: Proceedings of ETC 2015, Von Karman Institute for Fluid Dynamics, Rhode-St-Genèse - Belgium.
6.Gherardo ZAMBONINI, Xavier OTTAVYorcid_16x16.png (2015).
Unsteady preßure investigations of corner separated flow in a linear compreßor cascade
ASME Turbo Expo 2015, Montreal, Canada. doi:10.1115/GT2015-42073 doi.ico
In: Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, ASME, New York, USA. doi:10.1115/GT2015-42073 doi.ico
7.Johannes SCHREIBER, Xavier OTTAVYorcid_16x16.png, Ghislaine NGO BOUM, Stéphane AUBERT, Frédéric SICOT (2015).
Numerical simulation of the flow field in a high speed multistage compressor-Study of the time discretization sensitivity
ASME Turbo Expo 2015, Montreal, Canada. doi:10.1115/GT201542114 doi.ico
In: Proceedings of the ASME Turbo Expo 2015: Turbine Technical Conference and Exposition, ASME, New York, USA, 113665. doi:10.1115/GT201542114 doi.ico
8.Wei MA, Feng GAO, Xavier OTTAVYorcid_16x16.png, Lipeng LU, J. TENG (2014).
Influence factors on the turbulent boundary layer at mid-span in a linear compressor cascade
5th International Symposium on Jet Propulsion and Power Engineering, Beijing, China.
In: Proceedings of ISJPPE 5, , .
9.Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png (2014).
Study of the acoustic resonance occurring in a multistage highspeed axial compressor
10th European Conference on Turbomachinery Fluid Dynamics and Thermodynamics, Lappeenranta, Finland.
In: Proceedings of ETC 10, Von Karman Institute for Fluid Dynamics, Rhode-St-Genèse - Belgium, 446–458.
10.Feng GAO, Gherardo ZAMBONINI, Wei MA, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Liang SHAOorcid_16x16.png (2014).
Turbulent dynamics in a linear compressor cascade
5th International Symposium on Jet Propulsion and Power Engineering, Beijing, China.
In: Proceedings of ISJPPE 5, , , 2014-ISJPPE-5017.
11.Feng GAO, Wei MA, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Francis LEBOEUF (2013).
Numerical analysis of three-dimensional corner separation in a linear compressor cascade
ASME Turbo Expo 2013, San Antonio, United States. doi:10.1115/GT2013-95581 doi.ico
In: Proceedings of the ASME Turbo Expo 2013, ASME, New York, USA, GT2013-95581. doi:10.1115/GT2013-95581 doi.ico
12.Feng GAO, Wei MA, Jérôme BOUDETorcid_16x16.png, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Francis LEBOEUF (2012).
Numerical simulation of three-dimensional separated flow in a linear compressor cascade
4th International Symposium on Jet Propulsion and Power Engineering, Xian, China.
In: Proceedings of ISJPPE 2012, , .
13.Mehmet MERSINLIGIL, Jean-François BROUCKAERT, Nicolas COURTIADE, Xavier OTTAVYorcid_16x16.png (2011).
A high temperature high bandwidth fast response total pressure probe for measurements in a multistage axial compressor
ASME Turbo Expo 2011, Vancouver, Canada.
In: Proceedings of ASME Turbo Expo 2011 - GT2011, ASME, New York, USA.
GT2011-45558
14.Wei MA, Xavier OTTAVYorcid_16x16.png, Lipeng LU, Francis LEBOEUF, Feng GAO (2011).
Experimental investigations of corner stall in a linear compressor cascade
ASME Turbo Expo 2011, Vancouver, Canada.
In: Proceedings of ASME Turbo Expo 2011 - GT2011, ASME, New York, USA.
GT2011‑45236
15.Isabelle TRÉBINJAC, Nicolas BULOT, Xavier OTTAVYorcid_16x16.png, Nicolas BUFFAZ (2011).
Surge inception in a transonic centrifugal compressor stage
ASME Turbo Expo 2011, Vancouver, Canada.
In: Proceedings of ASME Turbo Expo 2011 - GT2011, ASME, New York, USA.
GT2011‑45116
16.Guillaume LEGRAS, Nicolas GOURDAIN, Isabelle TRÉBINJAC, Xavier OTTAVYorcid_16x16.png (2011).
Analysis of unsteadiness on casing treatment mechanisms in an axial compressor
ASME Turbo Expo 2011, Vancouver, Canada.
In: Proceedings of ASME Turbo Expo 2011 - GT2011, ASME, New York, USA.
GT2011-45806
17.Francis LEBOEUF, Isabelle TRÉBINJAC, Xavier OTTAVYorcid_16x16.png, Nicolas GOURDAIN (2010).
Aerodynamic studies in high-speed compressors dedicated to aeronautical applications
27th Congress of the International Council of the Aeronautical Sciences, Nice, France.
In: ICAS 2010 Proceedings, , .
18.Amadou C. SALL, Fabrice THOUVEREZ, Laurent BLANC, Pierrick JEAN, Xavier OTTAVYorcid_16x16.png (2010).
Prediction of the vibratory behaviour of monoblock sectorised stator vanes
ASME Turbo Expo 2010 : Power for Land, Sea and Air, GT 2010, Vancouver, Canada. doi:10.1115/GT2010-22698 doi.ico
In: Proceedings of the ASME Turbo Expo 2010, ASME, New York, USA, GT-2010-22698. doi:10.1115/GT2010-22698 doi.ico
19.Isabelle TRÉBINJAC, Xavier OTTAVYorcid_16x16.png, Nicolas ROCHUON, Nicolas BULOT (2009).
On the validity of steady calculations with shock-blade row interaction in compressors
9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Gyeongju, Korea, Republic of.
In: Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, , , ISAIF9-062.
20.Nicolas BULOT, Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC (2009).
Unsteady pressure measurements in a high-speed centrifugal compressor
9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Gyeongju, Korea, Republic of.
In: Proceedings of the 9th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, , , ISAIF9-066.
21.Nicolas BULOT, Isabelle TRÉBINJAC, Xavier OTTAVYorcid_16x16.png, Pascale KULISA, G. HALTER, Benoît PAOLETTI, Patrick KRIKORIAN (2009).
Experimental and numerical investigation of the flow field in a high-pressure centrifugal compressor impeller near surge
8th European Turbomachinery Conference, Graz, Austria.
In: Proceedings of the 8th European Conference on Turbomachinery, , , 447–458.
22.Nicolas GOURDAIN, Xavier OTTAVYorcid_16x16.png, André VOUILLARMET (2009).
Experimental and numerical investigation of unsteady flows in a high speed three stages compressor
8th European Turbomachinery Conference, Graz, Austria.
In: Proceedings of the 8th European Conference on Turbomachinery, , , 247–266.
23.Juliane BERTHIAU, Sébastien GOGUEY, Xavier OTTAVYorcid_16x16.png (2008).
Validation d?un système DGV à une caméra par mesures dans un jet circulaire bas subsonique
11e Congrès Francophone de Techniques Laser, Poitiers, France.
In: Actes du 11e Congrès Francophone de Techniques Laser, Association Francophone de Vélocimètrie Laser, ENSMA, BP 40109 - F-86961 Futuroscope Cedex, 465–476.
24.Juliane BERTHIAU, Sébastien GOGUEY, Xavier OTTAVYorcid_16x16.png (2008).
Development of a 1−camera Doppler Global Velocimmeter - First measurement in an round free jet
XIX Biannual symposium on measuring techniques in turbomachinery, Rhode-Saint-Genèse, Belgium.
In: G. PANIAGUA (Ed.), Proceedings of the XIX Biannual symposium on measuring techniques in turbomachinery, Von Karman Institute for Fluid Dynamics, Rhode-St-Genèse - Belgium.
25.Juliane BERTHIAU, Sébastien GOGUEY, Xavier OTTAVYorcid_16x16.png (2007).
Development of a 1−camera Doppler Global Velocimmeter
8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, Lyon, France.
In: Proceedings of the 8th International Symposium on Experimental and Computational Aerothermodynamics of Internal Flows, , , ISAIF8−00138.
26.D. ARNAUD, Xavier OTTAVYorcid_16x16.png, André VOUILLARMET (2004).
Experimental Investigation of the Rotor-Stator Interactions, Within a High-Speed, Multi-Stage, Axial Compressor: Part 2 - Modal Analysis of the Interactions
ASME Turbo Expo 2004 : Power for Land, Sea, and Air (GT2004), Vienne, Austria.
In: Proceedings of ASME Turbo Expo 2004 : Power for Land, Sea, and Air, ASME, New York, USA, GT2004-53778.
27.D. ARNAUD, Xavier OTTAVYorcid_16x16.png, André VOUILLARMET (2004).
Experimental Investigation of the Rotor-Stator Interactions Within a High Speed, Multi-Stage, Axial Compressor: Part 1 - Experimental Facilities and Results
ASME Turbo Expo 2004 : Power for Land, Sea, and Air (GT2004), Vienne, Austria.
In: Proceedings of ASME Turbo Expo 2004 : Power for Land, Sea, and Air, ASME, New York, USA, GT2004-53764.
 
communications sans actes
1.D. ARNAUD, Xavier OTTAVYorcid_16x16.png, Isabelle TRÉBINJAC (2000).
Mesures par anémométrie laser L2F-2D et 3D en turbomachines : Traitement des distorsions optiques créées par des hublots courbes
7ème Congrès Francophone de Vélocimétrie Laser, Marseille, France.
 
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