 | Monter d'un niveau |
Al-Kebsi, A., Pena, D., Laurendeau, É., Mose, R., & Hoarau, Y. (août 2017). Multi-step level-set ice accretion simulation with the NSMB solver [Communication écrite]. 23e Congrès français de mécanique, Lille, France (14 pages). Lien externe
Boukor, M., Choimet, A., Laurendeau, É., & Gosselin, F. P. (2024). Flutter limitation of drag reduction by elastic reconfiguration. Physics of Fluids, 36(2), 021915 (11 pages). Lien externe
Blanchet, M., Bourgault-Cote, S., & Laurendeau, É. (juin 2023). Advancements in CHAMPS for Multi-Layer Ice Accretion on Aircraft [Communication écrite]. SAE International Conference on Icing of Aircraft, Engines, and Structures (ICE 2023), Vienna, Austria. Lien externe
Bilodeau-Berube, C., & Laurendeau, É. (juin 2023). Airfoil Stall modeling via Roughness Amplification Model Coupled to Correlation-Based Transition Model [Communication écrite]. AIAA AVIATION 2023 Forum, Reston, VA, USA. Lien externe
Bilodeau-Bérubé, C., Blanchet, M., & Laurendeau, É. (juin 2022). Comparison of a correlation-based transitional model coupled to SA and kw-SST turbulence models [Communication écrite]. AIAA AVIATION 2022 Forum, Chicago, Illinois, USA. Lien externe
Blanchet, M., Bourgault-Cote, S., & Laurendeau, É. (juin 2022). Conservative hyperbolic droplet solver for aircraft icing [Communication écrite]. AIAA AVIATION 2022 Forum, Chicago, Illinois, USA. Lien externe
Bourgault-Cote, S., Papillon Laroche, H., Blanchet, M., & Laurendeau, É. (juin 2022). Contribution to IPW1 by studying multi-layer icing convergence in 2D/2.5D [Communication écrite]. AIAA AVIATION 2022 Forum, Chicago, Illinois, USA. Lien externe
Barrouillet, B., Laurendeau, É., & Yang, H. (janvier 2021). On the calibration of the transitional k-ω-γ-Reθt turbulence model [Communication écrite]. 2021 AIAA Scitech Forum (12 pages). Lien externe
Barrouillet, B., Laurendeau, É., & Yang, H. (août 2021). Optimized cross flow transition model for Reynolds Averaged Navier Stokes applications [Communication écrite]. AIAA Aviation 2021 Forum. Lien externe
Bourgault-Cote, S., Docampo-Sanchez, J., & Laurendeau, É. (2019). Multilayer Airfoil Ice Accretion Simulations Using a Level-Set Method with B-Spline Representation. AIAA Journal, 57(8), 3299-3308. Lien externe
Bourgault-Cote, S., Parenteau, M., & Laurendeau, É. (mars 2019). Quasi-3D multi-layer ice accretion model using a Vortex Lattice Method combined with 2.5D RANS solutions [Communication écrite]. 54th 3AF International Conference on Applied Aerodynamics, Paris, France (7 pages). Non disponible
Bourgault-Cote, S., Docampo-Sánchez, J., & Laurendeau, É. (janvier 2018). Multi-layer ice accretion simulations using a level-set method with B-spline representation [Communication écrite]. AIAA Aerospace Sciences Meeting, Kissimmee, Florida. Lien externe
Bourgault-Côté, S., Ghasemi, S., Mosahebi, A., & Laurendeau, É. (2017). Extension of a two-dimensional Navier-Stokes solver for infinite swept flow. AIAA Journal, 55(2), 662-667. Lien externe
Bourgault-Cote, S., Hasanzadeh, K., & Laurendeau, É. (juillet 2017). Multi-layer icing methodologies for conservative ice growth [Communication écrite]. 7th European Conference for Aeronautics and Aerospace Science (EUCASS 2017), Milan, Italy (15 pages). Lien externe
Bagade, P., Laurendeau, É., Bhole, A., Sharma, N., & Sengupta, T. K. (décembre 2014). Comparison of RANS and DNS for Transitional Flow Over WTEA-TE1 Airfoil [Communication écrite]. IUTAM Symposium on Advances in Computation, Modeling and Control of Transitional and Turbulent Flows, Goa, India. Lien externe
Bourgault-Cote, S., & Laurendeau, É. (janvier 2015). Two-Dimensional/Infinite Swept Wing Ice Accretion Model [Communication écrite]. 53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida (13 pages). Lien externe
Chrust, M., Laurendeau, É., & Ostiguy, L. (2015). Accelerating low-fidelity aerodynamic codes on multi- and many-core architectures. Journal of Supercomputing, 71(9), 3456-3481. Lien externe
Deloze, T., & Laurendeau, É. (janvier 2014). NSMB contribution to the 2nd High Lift Prediction Workshop [Communication écrite]. 52nd AIAA Aerospace Sciences Meeting (SciTech 2014), National Harbor, Maryland. Lien externe
Elices Paz, P., Radenac, E., Peron, S., Blanchard, G., Laurendeau, É., & Villedieu, P. (juin 2023). 3D Immersed Boundary Methods for the Calculations of Droplet Trajectories towards Icing Application [Communication écrite]. SAE International Conference on Icing of Aircraft, Engines, and Structures (ICE 2023), Vienna, Austria. Lien externe
Fernandez-Escudero, C., Prothin, S., Laurendeau, É., Ross, A., & Michon, G. (2023). Nonlinear flap for passive flutter control of bidimensional wing. JVC/Journal of Vibration and Control. Lien externe
Fernandez-Escudero, C., Gagnon, M., Laurendeau, É., Prothin, S., Ross, A., & Michon, G. (janvier 2019). Experimental and Numerical Aeroelastic Analysis of Airfoil-Aileron System with Nonlinear Energy Sink [Communication écrite]. 37th IMAC, A Conference and Exposition on Structural Dynamics, Orlando, FL, United states. Lien externe
Fernandez-Escudero, C., Gagnon, M., Laurendeau, É., Prothin, S., Michon, G., & Ross, A. (2019). Comparison of low, medium and high fidelity numerical methods for unsteady aerodynamics and nonlinear aeroelasticity. Journal of Fluids and Structures, 91, 12 pages. Lien externe
Ferlisi, C. A., Mazzini, C.-F., Laurendeau, É., Ramasawmy, D. R., Da Ronch, A., & Stalnov, O. (janvier 2016). Case Study of Two Capstone Student Projects from Canada and the United Kingdom [Communication écrite]. 54th AIAA Aerospace Sciences Meeting (AIAA SciTech 2016), San Diego, California. Lien externe
Gu, X., Vo, H. D., Mureithi, N. W., & Laurendeau, É. (2022). Plasma gurney flap flight control at low angle of attack. Journal of Aircraft, 60(1), 172-189. Lien externe
Grozdanov, A., & Laurendeau, É. (juin 2017). Transonic aeroelasticity using the 2.5d non-linear vortex-lattice method [Communication écrite]. 17th International Forum on Aeroelasticity and Structural Dynamics (IFASD 2017), Como, Italy. Non disponible
Gallay, S., & Laurendeau, É. (2016). Preliminary-design aerodynamic model for complex configurations using lifting-line coupling algorithm. Journal of Aircraft, 53(4), 1145-1159. Lien externe
Gallay, S., & Laurendeau, É. (2015). Nonlinear Generalized Lifting-Line Coupling Algorithms for Pre/Poststall Flows. AIAA Journal, 53(7), 1784-1792. Lien externe
Gallay, S., Ghasemi, S., & Laurendeau, É. (janvier 2014). Sweep effects on non-linear lifting line theory near stall [Communication écrite]. 52nd AIAA Aerospace Sciences Meeting (SciTech 2014), National Harbor, Maryland. Lien externe
Ghasemi, S., Mosahebi, A., & Laurendeau, É. (janvier 2014). A two-dimensional/infinite swept wing navier-stokes solver [Communication écrite]. 52nd AIAA Aerospace Sciences Meeting (SciTech 2014), National Harbor, Maryland. Lien externe
Gariepy, M., Malouin, B., Trépanier, J.-Y., & Laurendeau, É. (2013). Far-field drag decomposition applied to the drag prediction workshop 5 cases. Journal of Aircraft, 50(6), 1822-1831. Lien externe
Gariepy, M., Malouin, B., Trépanier, J.-Y., & Laurendeau, É. (juin 2013). Far-field drag decomposition method applied to the DPW-5 test cases results [Communication écrite]. 31st AIAA Applied Aerodynamics Conference, San Diego, CA, United states. Lien externe
Hasanzadeh, K., Laurendeau, É., Castonguay, P., & Leblond, D. (juin 2017). A framework for multi-block structured grid smoothing algorithms for aircraft configurations [Communication écrite]. 23rd AIAA Computational Fluid Dynamics Conference, 2017, Denver, CO, United states. Lien externe
Hasanzadeh, K., Laurendeau, É., & Paraschivoiu, I. (2016). Grid-generation algorithms for complex glaze-ice shapes Reynolds-averaged Navier-Stokes simulations. AIAA Journal, 54(3), 847-860. Lien externe
Hoarau, Y., Pena, D., Vos, J. B., Charbonier, D., Gehri, A., Braza, M., Deloze, T., & Laurendeau, É. (janvier 2016). Recent Developments of the Navier Stokes Multi Block (NSMB) CFD solver [Communication écrite]. 54th AIAA Aerospace Sciences Meeting (AIAA SciTech 2016), San Diego, California. Lien externe
Hasanzadeh, K., Laurendeau, É., & Paraschivoiu, I. (janvier 2015). Adaptive curvature control grid generation algorithms for complex glaze ice shapes RANS simulations [Communication écrite]. 53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida (31 pages). Lien externe
Hasanzadeh, K., Pena, D., Hoarau, Y., & Laurendeau, É. (juin 2015). Multi-time Step Icing Calculations Using a 3D Multi-block Structured Mesh Generation Procedure [Communication écrite]. SAE International Conference on Icing of Aircraft, Engines, and Structures (ICE 2015), Prague, Czech republic. Lien externe
Hasanzadeh, K., Laurendeau, É., & Paraschivoiu, I. (2013). Quasi-steady convergence of multistep navier-stokes icing simulations. Journal of Aircraft, 50(4), 1261-1274. Lien externe
Hasanzadeh, K., Mosahebi, A., Laurendeau, É., & Paraschivoiu, I. (juin 2013). Validation and verification of multi-steps icing calculation using CANICE2D-NS code [Communication écrite]. 31st AIAA Applied Aerodynamics Conference, San Diego, CA, United states (28 pages). Lien externe
Kontogiannis, A., & Laurendeau, É. (2021). Adjoint state of nonlinear vortex-lattice method for aerodynamic design and control. AIAA Journal, 59(4), 1184-1195. Lien externe
Kontogiannis, A., Parenteau, M., & Laurendeau, É. (janvier 2019). Viscous-Inviscid Analysis of Transonic Swept Wings using 2.5D RANS and Parametric Shapes [Communication écrite]. AIAA Scitech Forum, San Diego, California. Lien externe
Linguori, V., Moens, F., Peter, J., & Laurendeau, É. (mars 2023). Aircraft fuselage effects on transonic wing pressure via non-linear vortex lattce method [Communication écrite]. 57th 3AF International Conference on Applied aerodynamics, Bordeaux, France (10 pages). Lien externe
Lavoie, P., Radenac, E., Blanchard, G., Laurendeau, É., & Villedieu, P. (2022). Immersed Boundary Methodology for Multistep Ice Accretion Using a Level Set. Journal of Aircraft, 59(4), 912-926. Lien externe
Lavoie, P., Radenac, E., Blanchard, G., Laurendeau, É., & Villedieu, P. (janvier 2021). A penalization method for eulerian droplet impingement simulations towards icing applications [Communication écrite]. AIAA Scitech Forum. Lien externe
Lavoie, P., Radenac, E., Blanchard, G., Laurendeau, É., & Villedieu, P. (août 2021). An Immersed Boundary Methodology for Multi-Step Ice Accretion using a Level-Set [Communication écrite]. AIAA Aviation and Aeronautics Forum and Exposition (AIAA AVIATION Forum 2021). Lien externe
Liguori, V., Plante, F., & Laurendeau, É. (janvier 2021). Implementation of an efficient Selective Frequency Damping method in a RANS solver [Communication écrite]. 2021 AIAA Scitech Forum. Lien externe
Lavoie, P., Radenac, E., Blanchard, G., Laurendeau, É., & Villedieu, P. (2021). An improved characteristic based volume penalization method for the Euler equations towards icing applications. Computers & Fluids, 222, 104917 (17 pages). Lien externe
Lavoie, P., Radenac, E., Blanchard, G., Laurendeau, É., & Villedieu, P. (2021). Penalization Method for Eulerian Droplet Impingement Simulations Toward Icing Applications. AIAA Journal, 60(2), 641-653. Lien externe
Liguori, V., Papillon-Laroche, H., Parenteau, M., & Laurendeau, É. (janvier 2020). Design and Development of a Computational Fluid Dynamics Software in the Context of a Capstone Project [Communication écrite]. AIAA Scitech 2020 Forum, Orlando, Florida. Lien externe
Lavoie, P., Blanchard, G., Radenac, E., Laurendeau, É., & Villedieu, P. (juin 2019). A Penalization Method for 2D Ice Accretion Simulations [Communication écrite]. SAE International Conference on Icing of Aircraft, Engines, and Structures, (ICE 2019), Minneapolis, MN, United states. Lien externe
Lavoie, P., Pena, D., Hoarau, Y., & Laurendeau, É. (2018). Comparison of thermodynamic models for ice accretion on airfoils. International Journal of Numerical Methods for Heat and Fluid Flow, 28(5), 1004-1030. Lien externe
Lashkajani, K. H., Laurendeau, É., Castonguay, P., & Leblond, D. (juin 2017). Framework of Multiblock Structured Grid Smoothing Algorithms for Aircraft Configurations [Communication écrite]. 23rd AIAA Computational Fluid Dynamics Conference / AIAA Aviation and Aeronautics Forum and Exposition, Denver, CO. Publié dans Journal of Aircraft, 55(4). Lien externe
Lavoie, P., Bourgault-Côté, S., & Laurendeau, É. (2018). Numerical algorithms for infinite swept wing ice accretion. Computers & Fluids, 161, 189-198. Lien externe
Levesque, A. T., Pigeon, A., Deloze, T., & Laurendeau, É. (janvier 2015). An overset grid 2D/infinite swept wing URANS solver using recursive cartesian virtual grid method [Communication écrite]. 53rd AIAA Aerospace Sciences Meeting, Kissimmee, Florida (15 pages). Lien externe
Merabet, R., & Laurendeau, É. (2022). Numerical simulations of a rotor in confined areas including the presence of wind. Aerospace Science and Technology, 126, 107657 (18 pages). Lien externe
Merabet, R., & Laurendeau, É. (juin 2021). Actuator line method for helicopter rotors computations in various flight conditions [Communication écrite]. 65th Aeronautics Conference (AERO 2021) (15 pages). Lien externe
Merabet, R., & Laurendeau, É. (2021). Hovering Helicopter Rotors Modeling Using the Actuator Line Method. Journal of Aircraft, 59(3), 774-787. Lien externe
Merabet, R., & Laurendeau, É. (janvier 2019). Parametric Study on the Velocity Sampling Techniques for the Actuator Line Method in 2D [Communication écrite]. AIAA Scitech Forum, San Diego, California. Lien externe
Mosahebi, A., & Laurendeau, É. (2017). A thorough study on the temporal accuracy of ALE-URANS solvers with and without respecting geometric conservation law. Journal of Aerospace Engineering and Mechanics, 1(2), 99-109. Non disponible
Malouin, B., Trépanier, J.-Y., & Laurendeau, É. (2016). Installation and interference drag decomposition via RANS far-field methods. Aerospace Science and Technology, 54, 132-142. Lien externe
Mosahebi, A., & Laurendeau, É. (2015). Convergence Characteristics of Fully and Loosely Coupled Numerical Approaches for Transition Models. AIAA Journal, 53(5), 1399-1404. Lien externe
Malouin, B., Gariepy, M., Trépanier, J.-Y., & Laurendeau, É. (2015). Engine pre-entry thrust and standard net thrust evaluation based on the far-field method. Aerospace Science and Technology, 45, 50-59. Lien externe
Malouin, B., Gariepy, M., Trépanier, J.-Y., & Laurendeau, É. (2015). Internal drag evaluation for a through-flow nacelle using a far-field approach. Journal of Aircraft, 52(6), 1847-1857. Lien externe
Mosahebi, A., & Laurendeau, É. (2015). Introduction of a modified segregated numerical approach for efficient simulation of γ-R̃eθt transition model. International Journal of Computational Fluid Dynamics, 29(6-8), 357-375. Lien externe
Masson, C., Veilleux, C., Laurendeau, É., & Paraschivoiu, I. (juin 1999). Accurate induced drag predictions over wing mounted on a fuselage operating in the transonic regime [Communication écrite]. 17th AIAA Applied Aerodynamics Conference. Collection of Technical Papers, Norfolk, VA. Lien externe
Nguyen, M. T., Castonguay, P., & Laurendeau, É. (2019). GPU parallelization of multigrid RANS solver for three-dimensional aerodynamic simulations on multiblock grids. Journal of Supercomputing, 75(5), 2562-2583. Lien externe
Nguyen, M. T., Castonguay, P., & Laurendeau, É. (juillet 2018). GPUs accelerated three-dimensional RANS solver for aerodynamic simulations on multiblock grids [Communication écrite]. 10th International Conference on Computational Fluid Dynamics (ICCFDU 2018), Barcelona, Spain. Lien externe
Proulx-Cabana, V., Michon, G., & Laurendeau, É. Parametrization Effects of the Non-Linear Unsteady Vortex Method with Vortex Particle Method for Small Rotor Aerodynamics [Communication écrite]. Non spécifié (58 pages). Lien externe
Papillon Laroche, H., Radenac, E., & Laurendeau, É. (2023). Stochastic ice accretion model using an unstructured advancing front technique. International Journal of Multiphase Flow, 163, 104420 (18 pages). Lien externe
Plante, F., & Laurendeau, É. (juin 2022). CHAMPS Contributions to the Fourth High Lift Prediction Workshop [Communication écrite]. AIAA AVIATION Forum, Chicago, IL, USA. Lien externe
Proulx-Cabana, V., Nguyen, M. T., Prothin, S., Michon, G., & Laurendeau, É. (2022). A Hybrid Non-Linear Unsteady Vortex Lattice-Vortex Particle Method for Rotor Blades Aerodynamic Simulations. Fluids, 7(2), 30 pages. Lien externe
Peng, W., Zhang, Y., Laurendeau, É., & Desmarais, M. C. (2022). Learning aerodynamics with neural network. Scientific Reports, 12(1), 6779 (10 pages). Lien externe
Plante, F., & Laurendeau, É. (juin 2021). Matrix-free global stability analysis framework for 2D and 3D applications [Communication écrite]. AIAA AVIATION 2022 Forum, Chicago, Illinois, USA. Lien externe
Parenteau, M., Bourgault-Cote, S., Plante, F., Kayraklioglu, E., & Laurendeau, É. (janvier 2021). Development of parallel CFD applications with the Chapel Programming Language [Communication écrite]. AIAA Scitech 2021 Forum. Lien externe
Papillon Laroche, H., Bourgault-Côté, S., Parenteau, M., & Laurendeau, É. (juin 2021). Development of an aircraft aero-icing suite using chapel programming language [Communication écrite]. 8th annual Chapel Implementers and Users Workshop (CHIUW 2021). Lien externe
Plante, F., Laurendeau, É., & Dandois, J. (janvier 2021). Lift cell prediction using a lifting-surface model [Communication écrite]. 2021 AIAA Scitech Forum. Lien externe
Papillon Laroche, H., Bourgault-Cote, S., & Laurendeau, É. (août 2021). Multi-Layer Stochastic Ice Accretion Model for Aircraft Icing [Communication écrite]. AIAA Aviation 2021 Forum. Lien externe
Plante, F., Laurendeau, É., & Dandois, J. (2021). Stall Cell Prediction Using a Lifting-Surface Model. AIAA Journal, 11 pages. Lien externe
Parenteau, M., & Laurendeau, É. (2021). A transonic, viscous nonlinear frequency domain Vortex Lattice Method for aeroelastic analyses. Journal of Fluids and Structures, 107, 103406 (26 pages). Lien externe
Prakash, A., & Laurendeau, É. (2020). Consistent surface roughness extension for wall functions. International Journal of Heat and Fluid Flow, 82, 11 pages. Lien externe
Parenteau, M., Bourgault-Cote, S., Plante, F., & Laurendeau, É. (mai 2020). Development of parallel CFD applications on distributed memory with chapel [Communication écrite]. 34th IEEE International Parallel and Distributed Processing Symposium Workshops (IPDPSW 2020), New Orleans, LA, USA. Lien externe
Parenteau, M., & Laurendeau, É. (2020). A general modal frequency-domain vortex lattice method for aeroelastic analyses. Journal of Fluids and Structures, 99, 13 pages. Lien externe
Plante, F., Dandois, J., Beneddine, S., Laurendeau, É., & Sipp, D. (2020). Link between subsonic stall and transonic buffet on swept and unswept wings: from global stability analysis to nonlinear dynamics. Journal of Fluid Mechanics, 908, A16 (40 pages). Lien externe
Plante, F., Dandois, J., & Laurendeau, É. (janvier 2019). Similarities Between Cellular Patterns Occurring in Transonic Buffet and Subsonic Stall [Résumé]. AIAA Science and Technology Forum and Exposition (AAIA SciTech) / AIAA Guidance, Navigation, and Control Conference, San Diego, CA. Publié dans AIAA Journal, 58(1). Lien externe
Plante, F., Dandois, J., & Laurendeau, É. (janvier 2019). Similitude between 3D cellular patterns in transonic buffet and subsonic stall [Communication écrite]. AIAA Scitech Forum, San Diego, California. Lien externe
Prakash, A., & Laurendeau, É. (juin 2019). A wall function approach to account for rough surface heat transfer in Spalart-Allmaras turbulence model [Communication écrite]. AIAA Aviation 2019 Forum, Reston, VA (23 pages). Lien externe
Plante, F., & Laurendeau, É. (2018). Acceleration of Euler and RANS solvers via Selective Frequency Damping. Computers & Fluids, 166, 46-56. Lien externe
Parenteau, M., Laurendeau, É., & Carrier, G. (2018). Combined high-speed and high-lift wing aerodynamic optimization using a coupled VLM-2.5D RANS approach. Aerospace Science and Technology, 76, 484-496. Lien externe
Parenteau, M., & Laurendeau, É. (2018). Nonlinear frequency-domain solver for vortex lattice method. AIAA Journal, 56(6), 2242-2251. Lien externe
Plante, F., & Laurendeau, É. (2018). Simulation of Transonic Buffet Using a Time-Spectral Method. AIAA Journal, 57(3), 1275-1287. Lien externe
Parenteau, M., Sermeus, K., & Laurendeau, É. (janvier 2018). VLM coupled with 2.5D RANS sectional data for high-lift design [Communication écrite]. AIAA Aerospace Sciences Meeting, Kissimmee, Florida. Lien externe
Plante, F., Dandois, J., & Laurendeau, É. (septembre 2018). ZDES and URANS Simulations of 3D Transonic Buffet Over Infinite Swept Wings [Communication écrite]. 7th Symposium on Hybrid RANS-LES Methods, Berlin, Germany. Lien externe
Plante, F., Laurendeau, É., Dandois, J., & Sartor, F. (juin 2017). Study of three-dimensional transonic buffet on swept wings [Communication écrite]. 35th AIAA Applied Aerodynamics Conference 2017, Denver, CO, United states (17 pages). Lien externe
Parenteau, M., Plante, F., Laurendeau, É., & Costes, M. (janvier 2017). Unsteady coupling algorithm for lifting-line methods [Communication écrite]. 55th AIAA Aerospace Sciences Meeting, Grapevine, Texas. Lien externe
Pena, D., Hoarau, Y., & Laurendeau, É. (2016). Development of a three-dimensional icing simulation code in the NSMB flow solver. International Journal of Engineering Systems Modelling and Simulation, 8(2), 86-98. Lien externe
Pena, D., Hoarau, Y., & Laurendeau, É. (2016). A single step ice accretion model using Level-Set method. Journal of Fluids and Structures, 65, 278-294. Lien externe
Pena, D., Deloze, T., Laurendeau, É., & Hoarau, Y. (septembre 2014). Icing modelling in NSMB with chimera overset grids [Communication écrite]. International Conference on Numerical Analysis and Applied Mathematics (ICNAAM-2014), Rhodes, Greece (4 pages). Lien externe
Robitaille, M., Mosahebi, A., & Laurendeau, É. (2015). Design of adaptive transonic laminar airfoils using the γ-R̃eθt transition model. Aerospace Science and Technology, 46, 60-71. Lien externe
Zayni, M. K., Blanchet, M., & Laurendeau, É. (mai 2023). Recent developements of the multi-physics solver champs-ice [Communication écrite]. Canadian Society for Mechanical Engineering International Congress (CSME 2023) & Computational Fluid Dynamics Canada Internation Congress (CFD 2023), Sherbrooke, Qc, Canada (6 pages). Lien externe
