PC
Paola Cinnella
93
Documents
Affiliations actuelles
Identifiants chercheurs
- paola-cinnella
- 0000-0001-9979-0783
- Google Scholar : https://scholar.google.fr/citations?user=wBRA0JAAAAAJ
- IdRef : 154697060
- ResearcherId : AAS-5304-2020
- ResearcherId : GXG-6743-2022
Publications
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AirfRANS: High Fidelity Computational Fluid Dynamics Dataset for Approximating Reynolds-Averaged Navier-Stokes Solutions36th Conference on Neural Information Processing Systems (NeurIPS 2022) Track on Datasets and Benchmarks, Nov 2022, New Orleans, United States
Communication dans un congrès
hal-03806092v3
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A high-order scheme for the numerical simulation of high-enthalpy hypersonic flowsEleventh International Conference on Computational Fluid Dynamics (ICCFD11), Jul 2022, Maui, United States
Communication dans un congrès
hal-03892605v1
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Assessment of a high-order implicit residual smoothing time scheme for multiblock curvilinear meshesInternational Conference on Computational Fluid Dynamics - ICCFD11, Jul 2022, Maui, United States
Communication dans un congrès
hal-03892610v1
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Application of high-order vorticity confinement schemes to turbulent flows55th 3AF International Conference on Applied Aerodynamics, Mar 2021, Poitiers, France
Communication dans un congrès
hal-03223226v1
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Data-Driven Deterministic Symbolic Regression of Nonlinear Stress-Strain Relation for RANS Turbulence Modelling2018 Fluid Dynamics Conference, 2018, Atlanta, Georgia, United States. pp.AIAA 2018-2900, ⟨10.2514/6.2018-2900⟩
Communication dans un congrès
hal-02170808v1
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Toward an improved wall treatment for multiple-correction k-exact schemes2018 Fluid Dynamics Conference, 2018, Atlanta, Georgia, United States. pp.AIAA 2018-4164, ⟨10.2514/6.2018-4164⟩
Communication dans un congrès
hal-02170821v1
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Vortical flow calculations using a high-order Vorticity Confinement method23rd AIAA Computational Fluid Dynamics Conference, Jun 2017, Denver, United States. ⟨10.2514/6.2017-3291⟩
Communication dans un congrès
hal-03449105v1
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Design methodology for supersonic ORC turbine bladesCFM 2017 - 23ème Congrès Français de Mécanique, Aug 2017, Lille, France
Communication dans un congrès
hal-03465279v1
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Investigation of the flow dynamics in a channel constricted by periodic hills45th AIAA Fluid Dynamics Conference, 2015, Dallas, United States. pp.2015-2480
Communication dans un congrès
hal-02156763v1
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Sensitivity of Supersonic ORC Turbine Injector Designs to Fluctuating Operating ConditionsASME TURBO EXPO 2015, 2015, Montreal, Canada. pp.V02BT39A012, ⟨10.1115/GT2015-42193⟩
Communication dans un congrès
hal-02156800v1
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Fast Design Methodology For Supersonic Turbines With Strong Real Gas EffectsCFM 2015 - 22ème Congrès Français de Mécanique, Aug 2015, Lyon, France
Communication dans un congrès
hal-03444925v1
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Assessment of time implicit discretizations for the computation of turbulent compressible flows22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, United States. pp.AIAA 2015-2754
Communication dans un congrès
hal-02156560v1
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Conservative and accurate method for turbomachinery stage interfacesCFM 2015 - 22ème Congrès Français de Mécanique, Aug 2015, Lyon, France
Communication dans un congrès
hal-03445039v1
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High order and conservative method for patched grid interfacesAIAA, Jun 2014, ATLANTA, United States
Communication dans un congrès
hal-01069453v1
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Numerical investigation of dense gas flows through transcritical multistage axial Organic Rankine Cycle turbinesCongrès français de mécanique (21 ; 2013 ; Bordeaux (Gironde), Aug 2013, France. pp.1-6
Communication dans un congrès
hal-00919470v1
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Modélisation quasi-dimensionnelle multizone de la phase de combustion dans un moteur à essence.Congrès français de mécanique (21 ; 2013 ; Bordeaux (Gironde))., Aug 2013, France. pp.1-6
Communication dans un congrès
hal-00878718v1
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Amélioration de la modélisation quasi dimensionnelle de la combustion dans les moteurs à essence : du modèle à deux zones au modèle multizonesCFM 2013 - 21ème Congrès Français de Mécanique, Aug 2013, Bordeaux, France
Communication dans un congrès
hal-03439865v1
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Toward improved simulation tools for compressible turbomachinery: assessment of RBC schemes for the transonic NASA Rotor 37 benchmark caseCongrès français de mécanique (21 ; 2013 ; Bordeaux (Gironde))., Aug 2013, France. pp.1-6
Communication dans un congrès
hal-00920571v1
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Numerical investigation of dense gas flows through transcritical multistage axial Organic Rankine Cycle turbinesCFM 2013 - 21ème Congrès Français de Mécanique, Aug 2013, Bordeaux, France
Communication dans un congrès
hal-03440450v1
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Toward improved simulation tools for compressible turbomachinery: assessment of residual-based compact schemes for the transonic NASA Rotor 37 benchmark caseCFM 2013 - 21ème Congrès Français de Mécanique, Aug 2013, Bordeaux, France
Communication dans un congrès
hal-03440584v1
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Efficient robust optimization techniques for uncertain dense gas flowsCFD & Optimization - ECCOMAS Thematic Conference, ECCOMAS, May 2011, Antalya, Turkey
Communication dans un congrès
inria-00591576v1
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Effets des approximations numériques et de la modélisation de la turbulence sur la dynamique fine échelle d'un tourbillon de Taylor-GreenCFM 2011 - 20ème Congrès Français de Mécanique, Aug 2011, Besançon, France
Communication dans un congrès
hal-03421204v1
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Simulation of real-gas flow with uncertainty analysis2nd International Workshops on Advances in Computational Mechanics, 2010, Yokohama, Japan
Communication dans un congrès
inria-00549379v1
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Nozzle Shape Optimization for Wet-Steam Flows19th AIAA Computational Fluid Dynamic Conference, 2009, San Antonio, United States
Communication dans un congrès
inria-00549325v1
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Quantification of thermodynamic uncertainties in real flows44eme Colloque d'Aérodynamique Appliquée, 2009, Nantes, France
Communication dans un congrès
inria-00549328v1
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Quantification of uncertainties in compressible flows with complex thermodynamic behavior39th AIAA Fluid Dynamic Conference, 2009, San Antonio, United States
Communication dans un congrès
inria-00549323v1
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Optimal Blade Shapes For Viscous Dense Gas Flows Through Turbine Cascades5th ECCOMAS, 2008, Venice, Italy
Communication dans un congrès
inria-00549371v1
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Efficient numerical simulation of three-dimensional Bethe-Zel'dovich-Thompson Fluid Flows5th ECCOMAS, 2008, Venice, Italy
Communication dans un congrès
inria-00549372v1
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Computationally Efficient Models For The Numerical Simulation Of Thermodynamically Complex Flows5th ECCOMAS, 2008, Venice, Italy
Communication dans un congrès
inria-00549356v1
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Accurate and Computationally Efficient Equations of State for the Numerical Simulation of Dense Gas Flows38th AIAA Fluid Dynamic Conference, 2008, Seattle, United States
Communication dans un congrès
inria-00549311v1
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Aerodynamic performance of turbulent dense gas flows past airfoils and wings5th ICCFD, 2008, Seoul, South Korea
Communication dans un congrès
inria-00549319v1
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Analysis and Optimization of Viscous Dense Gas Flow18h AIMETA Congress of Theoretical And Applied Mechanics, 2007, Brescia, Italy
Communication dans un congrès
inria-00549374v1
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GA-Hardness of Aerodynamic Optimization Problems: Analysis and Proposed Cures37th AIAA Fluid Dynamic Conference, 2007, Miami, United States
Communication dans un congrès
inria-00549310v1
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Optimal airfoil shapes for viscous dense gas flows36th AIAA Fluid Dynamic Conference, 2006, San Francisco, United States
Communication dans un congrès
inria-00549304v1
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GA-Hardness of dense-gas flow optimization problems15th IASTED International Conference on Applied Simulation and Modelling, 2006, Rhodes, Greece
Communication dans un congrès
inria-00549306v1
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Shape optimization for dense gas flows through turbine cascades4th International Conference on Computational Fluid Dynamics (ICCFD 4), 2006, Ghant, Belgium
Communication dans un congrès
inria-00549308v1
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Transonic BZT flows through turbine cascades3rd International Conference on Computational Fluid Dynamics, 2004, Toronto, Canada
Communication dans un congrès
inria-00549302v1
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A numerical solver for dense gas flows34h AIAA Fluid Dynamics Conference and Exhibit, 2004, Portland, United States
Communication dans un congrès
inria-00549298v1
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Investigation of BZT transonic flows past an airfoil using a 5th power virial equation of stateEuropean Conference on Computational Mechanics and Applied Sciences, 2004, Jyväskylä, Finland
Communication dans un congrès
inria-00549305v1
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Hot-Wire Anemometry in High Subsonic Organic Vapor FlowsAmerican Society of Mechanical Engineers, 2022, ⟨10.1115/GT2022-81686⟩
Proceedings/Recueil des communications
hal-03892667v1
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