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articles
1.Nicolas POUJOL, Martin BUISSON, Pierre DUQUESNEorcid_16x16.png, Isabelle TRÉBINJAC (2022).
Unsteady analysis of a pulsating alternate flow pattern in a radial vaned diffuser
Int. J. Turbomach. Propuls. Power 7, 23 (22 pages). doi:10.3390/ijtpp7030023 doi.ico clarivate_16x16.png
2.Pierre DUQUESNEorcid_16x16.png, Joffrey CHANÉAC, Gabriel MONDIN, Jérôme DOMBARD (2022).
Topology rule-based methodology for flow separation analysis in turbomachinery
Int. J. Turbomach. Propuls. Power 7, 21 (16 pages). doi:10.3390/ijtpp7030021 doi.ico clarivate_16x16.png
3.Valdo PAGÈS, Pierre DUQUESNEorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Laurent BLANC, Pascal FERRAND, Xavier OTTAVYorcid_16x16.png, Christoph BRANDSTETTERorcid_16x16.png (2022).
UHBR Open-Test-Case Fan ECL5/CATANA
Int. J. Turbomach. Propuls. Power 7, 17 (20 pages). doi:10.3390/ijtpp7020017 doi.ico clarivate_16x16.png
4.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 clarivate_16x16.png
5.Victor MOËNNE-LOCCOZ, Isabelle TRÉBINJAC, Nicolas POUJOL, Pierre DUQUESNEorcid_16x16.png (2020).
Detection and analysis of an alternate flow pattern in a radial vaned diffuser
Int. J. Turbomach. Propuls. Power 5, 2 (12 pages). doi:10.3390/ijtpp5010002 doi.ico hal.ico clarivate_16x16.png
6.Pierre DUQUESNEorcid_16x16.png, Quentin RENDU, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND (2019).
Choke flutter instability sources tracking with linearized calculations
Int. J. Numer. Methods Heat Fluid Flow 30, 4155–4166. doi:10.1108/HFF-06-2018-0281 doi.ico hal.ico clarivate_16x16.png
7.Victor MOËNNE-LOCCOZ, Isabelle TRÉBINJAC, Nicolas POUJOL, Pierre DUQUESNEorcid_16x16.png (2019).
Low frequency stall modes of a radial vaned diffuser flow
Mécanique et Industries 20, 805 (6 pages). doi:10.1051/meca/2020026 doi.ico hal.ico clarivate_16x16.png
8.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 clarivate_16x16.png
 
communications avec actes
1.Pierre DUQUESNEorcid_16x16.png, Bruno MAHIEUX, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND (2019).
Sensitivity of the aerodynamics damping coefficient prediction to the turbulence modelling conjugated with the vibration mode shape.
European Turbomachinery Conference (ETC 13), Lausanne, Switzerland.
In: Proceedings of 15th European Turbomachinery Conference (ETC 13), , .
2.Pierre DUQUESNEorcid_16x16.png, Quentin RENDU, Pascal FERRAND, Stéphane AUBERTorcid_16x16.png (2018).
Local contribution of blades vibration on the choke flutter instability in transonic UHBR fan
53rd 3AF International Conference on Applied Aerodynamics: Multiphysics approach in Aerodynamics, Salon-de-Provence, France.
In: proceedings of 53rd 3AF International Conference on Applied Aerodynamics: Multiphysics approach in Aerodynamics, , .
3.Pierre DUQUESNEorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Quentin RENDU, Pascal FERRAND (2018).
Effect of frozen turbulence assumption on the local blades vibration on the choke flutter instability in transonic UHBR fan
IUTAM Symposium on Critical flow dynamics involving moving/deformable structures with design applications, Santorini, Greece.
In: Proceedings of IUTAM Symposium on Critical flow dynamics involving moving/deformable structures with design applications, , .
4.Pierre DUQUESNEorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Quentin RENDU, D. FERRAND (2018).
Effect of nodal diameter on the local blades vibration on the choke flutter instability in transonic UHBR fan
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, , .
5.Christoph BRANDSTETTERorcid_16x16.png, Valdo PAGÈS, Pierre DUQUESNEorcid_16x16.png, Benoît PAOLETTI, Stéphane AUBERTorcid_16x16.png, 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. hal.ico
In: Proceedings of 15th International Symposium on Unsteady Aerodynamics, Aeroacoustics & Aeroelasticity of Turbomachines, , . hal.ico
 
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