Pierre Trontin
37
Documents
Publications
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Experimental and Numerical Investigation of Ice Crystal Icing on a Heatable NACA0012 AirfoilAIAA AVIATION 2022 Forum, Jun 2022, Chicago, United States. pp.AIAA 2022-3534, ⟨10.2514/6.2022-3534⟩
Conference papers
hal-03774073v1
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Supercooled large droplet (SLD) impact on ice at high velocity : splashing characterizationAIAA Aviation 2022 Forum, Jun 2022, Chicago, United States. ⟨10.2514/6.2022-4116⟩
Conference papers
hal-04039717v1
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Experimental and numerical investigations of snow accretionAIAA AVIATION 2021 FORUM, Aug 2021, Virtual event, United States. pp.AIAA 2021-2684, ⟨10.2514/6.2021-2684⟩
Conference papers
hal-03440994v1
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Semi-empirical Erosion Model with Particle Size and Liquid Water Content Effects for Ice Crystal Icing SimulationsAIAA AVIATION 2020, Jun 2020, RENO, United States. ⟨10.2514/6.2020-2827⟩
Conference papers
hal-02906383v1
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Ice crystals trajectory calculations in a turbofan engineAIAA AVIATION 2018, Jun 2018, ATLANTA, United States
Conference papers
hal-01895949v1
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A shallow water type model to describe the dynamic of thin partially wetting filmsCFM 2017 - 23ème Congrès Français de Mécanique, Aug 2017, Lille, France
Conference papers
hal-03465787v1
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Heat and mass transfer analogies for evaporation models at high evaporation rateAIAA AVIATION 2014, Jun 2014, ATLANTA, United States
Conference papers
hal-01069553v1
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A robust coupling algorithm applied to thermal ice protection system unsteady modeling6th AIAA Atmospheric and Space Environments Conference - AVIATION 2014, Jun 2014, ATLANTA, United States
Conference papers
hal-01088749v1
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Goal oriented mesh adaptation using total derivative of aerodynamic functions with respect to mesh coordinates50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, American Institute of Aeronautics and Astronautics (AIAA), Jan 2012, Nashville, Tennessee, United States
Conference papers
hal-00769601v1
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Goal oriented mesh adaptation using total derivative of aerodynamic functions with respect to mesh coordinates49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, American Institute of Aeronautics and Astronautics (AIAA), Jan 2011, Orlando, Florida, United States
Conference papers
hal-00769599v1
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Numerical Simulation of Electrothermal Ice Protection SystemsHandbook of Numerical Simulation of In-Flight Icing, Springer International Publishing, pp.1-79, 2023, ⟨10.1007/978-3-030-64725-4_16-1⟩
Book sections
hal-04206670v1
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Numerical Simulation of Ice Crystals and Mixed-Phase In-Flight Icing ConditionsHandbook of Numerical Simulation of In-Flight Icing, Springer International Publishing, pp.599-642, 2023, 978-3-031-33844. ⟨10.1007/978-3-031-33845-8_40⟩
Book sections
hal-04206671v1
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A Phase-Conditioned Filtering of Incompressible Interfacial Multiphase Flow Equations: A Priori Study for the Modeling of LES Subgrid Scale TermsTurbulence and Interactions, 125, Springer Berlin Heidelberg, pp.165-172, 2014, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, ⟨10.1007/978-3-662-43489-5_20⟩
Book sections
hal-03709342v1
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Direct numerical simulation of particle turbulence interaction in forced turbulenceNotes On Numerical Fluid Mechanics And Multidisciplinary Design, Springer, 2014
Book sections
hal-01860921v1
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An a Priori Study for the Modeling of Subgrid Terms in Multiphase FlowsTurbulence and Interactions, 110, Springer Berlin Heidelberg, pp.377-384, 2010, Notes on Numerical Fluid Mechanics and Multidisciplinary Design, ⟨10.1007/978-3-642-14139-3_46⟩
Book sections
hal-03709330v1
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Développement d'une approche de type LES pour la simulation d'écoulements diphasiques avec interface. Application à l'atomisation primaire.Physique [physics]. Ecole nationale superieure de l'aeronautique et de l'espace, 2009. Français. ⟨NNT : ⟩
Theses
tel-00499373v1
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Contribution to the development of models and numerical methods for fluid mechanics and icing problemsEngineering Sciences [physics]. UNIVERSITE DE TOULOUSE; Université Toulouse 3 Paul Sabatier (UT3 Paul Sabatier), 2019
Habilitation à diriger des recherches
tel-02365923v1
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