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articles
1.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 openalex-16x16.png
2.Zebin ZHANG, Martin BUISSON, Pascal FERRAND, Manuel HENNER (2021).
Integration of second-order sensitivity method and cokriging surrogate model
Mathematics 9, 401 (15 pages). doi:10.3390/math9040401 doi.ico hal.ico openalex-16x16.png
3.Quentin RENDU, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND (2020).
Numerical identification of mechanisms triggering 2D choke flutter in transonic fan
J. Fluids Struct. 97, 102879 (14 pages). doi:10.1016/j.jfluidstructs.2020.102879 doi.ico hal.ico openalex-16x16.png
4.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 openalex-16x16.png
5.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
6.Sandrine LABIT, Jean-Camille CHASSAING, Mickaël PHILIT, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND (2016).
Time-harmonic Navier-Stokes computations of forced shock-wave oscillations in a transonic nozzle
Comput. Fluids 127, 102–114. doi:10.1016/j.compfluid.2015.12.005 doi.ico hal.ico openalex-16x16.png
7.Zebin ZHANG, Martin BUISSON, Pascal FERRAND, Manuel HENNER, F. GILLOT (2015).
Meta-model based optimization of a large diameter semi-radial conical hub engine cooling fan
Mech. Ind. 16, 102 (8 pages). hal.ico
8.Martin BUISSON, Pascal FERRAND, Laurent SOULAT, Stéphane AUBERTorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Claire RAMBEAU, Manuel HENNER (2013).
Optimal design of an automotive fan using the Turb'Opty meta-model
Comput. Fluids 80, 207–213. doi:10.1016/j.compfluid.2012.03.015 doi.ico hal.ico openalex-16x16.png
9.Laurent SOULAT, Pascal FERRAND, Stéphane MOREAUorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, Martin BUISSON (2013).
Efficient optimisation procedure for design problems in fluid mechanics
Comput. Fluids 82, 73–86. doi:10.1016/j.compfluid.2013.04.009 doi.ico hal.ico openalex-16x16.png
10.Hakim FERRIA, Pascal FERRAND, François PACULL, Stéphane AUBERTorcid_16x16.png (2012).
Numerical investigation of flutter stability in subsonic space turbine blisk with emphasis on cut-on/cut-off modes and interblade phase angles
J. Therm. Sci. 21, 492–499. doi:10.1007/s11630-012-0573-y doi.ico openalex-16x16.png
11.Nicolas TAUVERON, Manuel SAEZ, Pascal FERRAND, Francis LEBOEUF (2007).
Axial turbomachine modelling with a 1D axisymmetric approach - Application to gas cooled nuclear reactor
Nucl. Eng. Des. 237, 1679–1692. doi:10.1016/j.nucengdes.2007.01.019 doi.ico openalex-16x16.png
12.P. HERONT, Pascal FERRAND, Francis LEBOEUF, E.M. EL GHAZZANI (1998).
Couplage entre un code de calcul méridien instationnaire et un code de calcul 3D dans l'optique de simuler les écoulements transitoires de démarrage dans les turbopompes multiétagées.
Houille Blanche-Rev. Int. 53, 16–22.
13.Pascal FERRAND, Stéphane AUBERTorcid_16x16.png (1998).
A new mixed AUSM + Liou scheme, an extention of the mixed Van Leer flux splitting.
C. r. Acad. sci., Sér. IIb Méc. 326, 5–11.
14.Pascal FERRAND (1997).
Le projet TUMULT, TUrbomachine MULTi-étages : Analyse des écoulements instationnaires.
Lettre d'information du CNUSC .
15.Pascal FERRAND, Stéphane AUBERTorcid_16x16.png (1996).
New mixed Van Leer flux splitting for transonic viscous flow.
AIAA J. 34, 190–193.
16.Stéphane AUBERTorcid_16x16.png, L. HALLO, Pascal FERRAND, Marc BUFFAT (1995).
Numerical simulation of a three-dimensional nozzle, from inviscid to turbulent flows.
Int. J. Numer. Methods Heat Fluid Flow 5, 889–905.
17.Stéphane AUBERTorcid_16x16.png, L. HALLO, Pascal FERRAND, Marc BUFFAT (1995).
Numerical behaviour of unsteady waves.
AIAA J. 33, 888–893.
18.Pascal FERRAND, Stéphane AUBERTorcid_16x16.png (1993).
Van Leer's flux splitting adaptation to increase spatial accuracy at low Mach numbers.
C. r. Acad. sci., Sér. IIb Méc. 317, 1–4.
 
thèses/hdr
1.Guillaume BÉNÉFICE (dir.: Pascal FERRAND, Yannick ROZENBERG) (2015).
Développement d'une méthode de couplage partitionné fort en vue d'une application aux turbomachines
Thèse École centrale de Lyon
2.William RIÉRA (dir.: Pascal FERRAND) (2014).
Evaluation of the ZDES method on an axial compressor: analysis of the effects of upstream wake and throttle on the tip-leakage flow
Thèse École centrale de Lyon
3.Pierre GOUGEON (dir.: Pascal FERRAND, Ghislaine NGO BOUM) (2014).
Étude des interactions aérodynamiques entre une turbine haute pression et le premier distributeur basse pression
Thèse École centrale de Lyon
4.Zebin ZHANG (dir.: Pascal FERRAND) (2014).
Intégration des méthodes de sensibilité d'ordre élevé dans un processus de conception optimale des turbomachines. Développement de méta-modèles
Thèse École centrale de Lyon
5.Florent PAYER (dir.: Pascal FERRAND) (2013).
Prédiction et analyse du phénomène de réponse forcée. Application à un cas de compresseur haute pression
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2393_fpayer.pdf
6.Mickaël PHILIT (dir.: Pascal FERRAND) (2013).
Modélisation, simulation et analyse des instationnarités en écoulement transsonique décollé en vue d'application à l'aéroélasticité des Turbomachines
Thèse École centrale de Lyon
7.Hakim FERRIA (dir.: Pascal FERRAND, T. H. FRANSSON) (2011).
Contribution to numerical and experimental studies of flutter in space turbines. Aerodynamic analysis of subsonic or supersonic flows in response to a prescribed vibratory mode of the structure
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/TH_T2243_hferria.pdf
8.Laurent SOULAT (dir.: Pascal FERRAND) (2010).
Définition, analyse et optimisation aérodynamique d'un nouveau concept de traitement de carter au moyen d'outils numériques. Application aux turbomachines basse vitesse
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/lsoulat.pdf
9.Nicolas TAUVERON (dir.: Pascal FERRAND, Francis LEBOEUF) (2006).
Simulation numérique et analyse du déclenchement et du développement des instabilités axiales dans les turbomachines. Application à un transitoire de brêche dans un réacteur nucléaire à hélium.
Thèse École centrale de Lyon
http://bibli.ec-lyon.fr/exl-doc/ntauveron.pdf
10.O. BRON (dir.: T. H. FRANSSON, Pascal FERRAND) (2004).
Etude expérimentale et numérique de l'interaction onde de choc - couche limite en écoulement transsonique instationnaire.
Thèse Kungliga Tekniska Högskolan Stockholm
11.Jérôme BOUDETorcid_16x16.png (dir.: Pascal FERRAND, Marc C. JACOB) (2003).
Approches numériques pour la simulation du bruit à large bande en vue de l'application aux turbomachines.
Thèse École centrale de Lyon
12.Jérôme TOURNIER (dir.: Pascal FERRAND) (2003).
Évaluation du couplage d'un algorithme d'optimisation avec une technique de paramétrisation appliquée à la mécanique des fluides.
Thèse École centrale de Lyon
 
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, 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, , .
3.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, , .
4.Guillaume BÉNÉFICE, Yannick ROZENBERG, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND, Fabrice THOUVEREZ (2014).
A Partitioned strong coupling procedure for simulation of shock wave / flexible structure interaction
ASME 2014 4th Joint US-European Fluids Engineering Division Summer Meeting (FEDSM 2014), Chicago, United States.
In: Proceedings of FEDSM 2014, ASME, New York, USA, FEDSM2014-21624.
5.Martin BUISSON, Pascal FERRAND, Laurent SOULAT, Stéphane AUBERTorcid_16x16.png, Stéphane MOREAUorcid_16x16.png, Claire RAMBEAU, Manuel HENNER (2012).
Turb'opty based optimization of a shrouded fan with casing treatment
28th Congress of the International Council of the Aeronautical Sciences, Brisbane, Australia.
In: Proceedings of ICAS 2012, Optimage Ltd, Edinburgh, Scotland, Paper ICAS 2012-4.4.4 .
full text
6.Mickaël PHILIT, Pascal FERRAND, Sandrine LABIT, Jean-Camille CHASSAING, Stéphane AUBERTorcid_16x16.png, T. H. FRANSSON (2012).
Derivated turbulence model to predict harmonic loads in transonic separated flows over a bump
28th Congress of the International Council of the Aeronautical Sciences, Brisbane, Australia.
In: Proceedings of ICAS 2012, Optimage Ltd, Edinburgh, Scotland, Paper ICAS 2012-4.6.4.
full text
7.Florent PAYER, Pascal FERRAND, Alain DUGEAI, Fabrice THOUVEREZ (2012).
Comparison of fluid-structure coupling methods for blade forced response prediction
ASME 2012 Gas Turbine India Conference, Mumbai, India. doi:10.1115/GTINDIA2012-9521 doi.ico
In: Proceedings of GTINDIA 2012, ASME, New York, USA, 595–602. doi:10.1115/GTINDIA2012-9521 doi.ico
8.Stéphane AUBERTorcid_16x16.png, Pascal FERRAND, François PACULL, Martin BUISSON (2010).
Fast CFD for shape and flow parameterization with meta-models built on high-order derivatives. Applications to fast design.
27th Congress of the International Council of the Aeronautical Sciences, Nice, France.
In: ICAS 2010 Proceedings, , .
9.Hakim FERRIA, François PACULL, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND, S. AKNOUCHE, B. POUFFARY (2009).
2D Elementary geometric decomposition to study flutter motion of a space turbine blisk
ASME Turbo Expo 2009: Power for Land, Sea and Air (TE09), Orlando, United States.
In: Proceedings of ASME Turbo Expo 2009 : Power for Land, Sea, and Air, ASME, New York, USA, GT2009-60032.
10.Laurent SOULAT, Pascal FERRAND, Stéphane AUBERTorcid_16x16.png, Stéphane MOREAUorcid_16x16.png (2009).
Numerical evaluation of a new casing treatment based on Holweck type vacuum pumps
8th European Turbomachinery Conference, Graz, Austria.
In: Proceedings of the 8th European Conference on Turbomachinery, , , ETC paper 089.
11.M. N\'DIAYE, G. GRONDIN, V. KELNER, Pascal FERRAND, Stéphane MOREAUorcid_16x16.png (2007).
Multi objective optimization of a blade fan using an advanced parametrization method
First CEAS European Air and Space Conference Century Perspectives, Berlin, Germany.
In: Proceedings of the First CEAS European Air and Space Conference Century Perspectives, CEAS, .
12.L. GAMET, Pascal FERRAND, Marc C. JACOBorcid_16x16.png (2007).
Noise prediction of fan-tip/boundary layer interaction
Third International Symposium Fan Noise 2007, Lyon, France. hal.ico
In: Proceedings of Fan Noise 2007, CETIAT, VILLEURBANNE. hal.ico
13.Stéphane MOREAUorcid_16x16.png, Stéphane AUBERTorcid_16x16.png, G. GRONDIN, Pascal FERRAND (2006).
Optimization of a fan blade cascade using the parametric flow solver Turb?opty
ASME 2006 Joint U.S.- European Fluids Engineering Summer Meeting, Miami, United States.
In: Proceedings of the ASME 2006 Joint U.S.-European Fluids Engineering Summer Meeting, ASME, New York, USA, FEDSM2006-98543.
14.Nicolas TAUVERON, Pascal FERRAND, Francis LEBOEUF (2006).
Simulation of surge inception and performance of axial multistage compressor
ASME Turbo Expo 2006 : Power for Land, Sea, and Air (GT2006), Barcelona, Spain.
In: Proceedings of ASME Turbo Expo 2006 : Power for Land, Sea, and Air, ASME, New York, USA.
15.Nicolas TAUVERON, Pascal FERRAND, Francis LEBOEUF (2006).
Dynamic modeling of a nuclear gas turbine plant. Application to surge prediction
ASME Turbo Expo 2006 : Power for Land, Sea, and Air (GT2006), Barcelona, Spain.
In: Proceedings of ASME Turbo Expo 2006 : Power for Land, Sea, and Air, ASME, New York, USA.
16.Pascal FERRAND, Jérôme BOUDETorcid_16x16.png, Joëlle CARO, Stéphane AUBERTorcid_16x16.png, Claire RAMBEAU (2006).
Analyses of URANS and LES capabilities to predict vortex shedding for rods and turbines
10th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT), Durham, United States. doi:10.1007/1-4020-4605-7_28 doi.ico
In: Kenneth C. HALL (Ed.), Robert E. KIELB (Ed.), Jeffrey P. THOMAS (Ed.), Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Springer, Dordrecht, The Netherlands, 381–393. doi:10.1007/1-4020-4605-7_28 doi.ico
17.Nicolas TAUVERON, Manuel SAEZ, Pascal FERRAND, Francis LEBOEUF (2005).
Axial turbomachine modelling with a 1D axisymmetric approach. Application to gas cooled nuclear reactor transients
NURETH 11, Avignon, France.
In: Proceedings of the 11th International Topical Meeting on Nuclear Reactor Thermal Hydraulics, American Nuclear Society, La Grange Park, Illinois, U.S.A., paper 460.
18.Nicolas TAUVERON, Pascal FERRAND, Francis LEBOEUF (2005).
Modélisation d'une turbomachine axiale multiétage selon une approche 1,5 D. Application au transitoire d'un réacteur nucléaire refroidi par gaz
40ème Colloque d'Aérodynamique Appliquée, Toulouse, France.
In: Actes du 40ème Colloque d'Aérodynamique Appliquée, Association Aéronautique & Astronautique de France (AAAF), .
19.G. GRONDIN, V. KELNER, Pascal FERRAND, Stéphane MOREAUorcid_16x16.png (2005).
Robust design and parametric performance study of an automotive fan blade by coupling multi-objective genetic optimization and flow parameterization
International Congress on Fluid Dynamics Applications in Ground Transportation, Lyon, France.
In: Proceedings of the International Congress of Fluid Dynamics Applications in Ground Transportation, SIA, .
20.Jérôme BOUDETorcid_16x16.png, Damiano CASALINO, Marc C. JACOBorcid_16x16.png, Pascal FERRAND (2004).
Prediction of broadband noise: airfoil in the wake of a rod
42nd AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, United States. doi:10.2514/6.2004-852 doi.ico hal.ico
In: Proceedings of the 42nd AIAA Aerospace Sciences Meeting and Exhibit, AIAA, Reston, Virginia, USA, AIAA-2004-0852. doi:10.2514/6.2004-852 doi.ico hal.ico
21.Jérôme BOUDETorcid_16x16.png, Damiano CASALINO, Marc C. JACOBorcid_16x16.png, Pascal FERRAND (2003).
Prediction of sound radiated by a rod using large-eddy simulation
9th AIAA/CEAS Aeroacoustics Conference, Hilton Head, United States. doi:10.2514/6.2003-3217 doi.ico hal.ico
In: Proceedings of the 9th AIAA/CEAS Aeroacoustics Conference, AIAA, Reston, Virginia, USA, AIAA-2003-3217. doi:10.2514/6.2003-3217 doi.ico hal.ico
22.Jérôme BOUDETorcid_16x16.png, Damiano CASALINO, Marc C. JACOBorcid_16x16.png, Pascal FERRAND (2002).
Unsteady RANS computations of the flow past an airfoil in the wake of a rod
ASME Fluids Engineering Division Summer Meeting 2002, Montreal, Canada. doi:10.1115/FEDSM2002-31343 doi.ico hal.ico
In: Proceedings of ASME Fluids Engineering Division Summer Meeting 2002, ASME, New York, USA, FEDSM2002-31343. doi:10.1115/FEDSM2002-31343 doi.ico hal.ico
23.G.L. OLIVEIRA, Pascal FERRAND, Stéphane AUBERTorcid_16x16.png (1999).
Numerical analysis of wakes interactions in a transonic inviscid flow of compressor
Third European Conference on Turbomachinery: fluid dynamics and thermodynamics, London, United Kingdom.
In: IMECHE Cconference Transactions, Institution of Mechanical Engineers, London, UJ, 333–342.
24.G.L. OLIVEIRA, Pascal FERRAND, Stéphane AUBERTorcid_16x16.png (1999).
Inlet wakes influence on axial transonic compressor performances
3rd ASME/JSME Joint Fluids Engineering Conference, FEDSM'99, San Francisco, United States.
In: Proceedings of FEDSM'99, ASME, New York, USA, 503–510.
 
communications sans actes
1.Yannick ROZENBERG, Pascal FERRAND, Mickaël PHILIT, Stéphane AUBERTorcid_16x16.png (2013).
On the use of radial basis functions to numerically predict flutter in turbomachinery
International Forum on Aeroelasticity and Structural Dynamics, Bristol, United Kingdom.
2.L. GAMET, Pascal FERRAND, Marc C. JACOBorcid_16x16.png (2007).
Noise prediction of fan-tip/boundary layer interaction
42éme Colloque d'Aérodynamique Appliquée : Couplages et optimisation multidisciplinaires, Nice, France.
3.M. N\'DIAYE, François PACULL, Stéphane AUBERTorcid_16x16.png, Pascal FERRAND (2007).
CFD parametrization technique for aero-structures illustrited with airfoil-flap configuration
2nd International Conference ?Supply on the wings?, Frankfurt, Germany.
4.Nicolas TAUVERON, Pascal FERRAND, Francis LEBOEUF (2006).
A numerical contribution to the analysis of surge inception and development in axial compressors
11th International Symposium on Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines (ISUAAAT), Moscow, Russian Federation.
 
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