Volume 39, Issue 3 No AccessAutomated Method for Transition Prediction on Wings in Transonic FlowsMarc Langlois, Christian Masson, Fassi Kafyeke and Ion ParaschivoiuMarc Langlois Bombardier Aerospace, Montreal, Quebec H4R 1K2, CanadaSearch for more papers by this author, Christian Masson Ecole de Technologie Superieure, Montreal, Quebec H3C 1K3, CanadaSearch for more papers by this author, Fassi Kafyeke Bombardier Aerospace, Montreal, Quebec H4R 1K2, CanadaSearch for more papers by this author and Ion Paraschivoiu Ecole Polytechnique de Montreal, Montreal, Quebec H3C 3A7, CanadaSearch for more papers by this authorPublished Online:22 May 2012https://doi.org/10.2514/2.2951SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookXLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited byNeural Networks as a Surrogate Model for Linear Stability Analysis of Three-Dimensional Compressible Boundary LayersPaul Hoffmann, Alexander Theiß and Stefan Hein4 January 2024Modeling of Transonic Transitional Three-Dimensional Flows for Aerodynamic ApplicationsAndrey V. Boiko, Kirill V. Demyanko, Stanislav V. Kirilovskiy, Yuri M. Nechepurenko and Tatiana V. Poplavskaya20 July 2021 | AIAA Journal, Vol. 59, No. 9Recurrent neural network for end-to-end modeling of laminar-turbulent transition19 October 2021 | Data-Centric Engineering, Vol. 2Convolutional neural network for transition modeling based on linear stability theory23 November 2020 | Physical Review Fluids, Vol. 5, No. 11Study on Cruise Drag Characteristics of Low Drag Normal Layout Civil Aircraft6 August 2020 | Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University, Vol. 38, No. 3Boundary-layer transition of advanced fighter wings at high-speed cruise conditions1 Apr 2019 | Chinese Journal of Aeronautics, Vol. 32, No. 4Parabolized Stability Equations Code with Automatic Inflow for Swept Wing Transition AnalysisL. Kosarev, S. Séror and Y. Lifshitz19 June 2016 | Journal of Aircraft, Vol. 53, No. 6Extensible Rapid Transition Prediction for Aircraft Conceptual Design Using Modal DecompositionDev Rajnarayan and Peter Sturdza5 January 2013Extensible Rapid Transition Prediction for Aircraft Conceptual DesignDev Rajnarayan and Peter Sturdza10 August 2012Automatic Transition Predictions Using Simplified Methods Jean Perraud , Daniel Arnal , Gregoire Casalis , Jean-Pierre Archambaud and Raffaele Donelli 2 May 2012 | AIAA Journal, Vol. 47, No. 11Automatic Transition Predictions using Simplified MethodsJean Perraud, Daniel Arnal, Gregoire Casalis, Jean-Pierre Archambaud and Raffaele Donelli15 June 2012 What's Popular Volume 39, Number 3May 2002 Metrics Crossmark TopicsAerodynamicsAerospace SciencesAircraft DesignAircraft Operations and TechnologyAircraft Wing DesignBoundary LayersComputational Fluid DynamicsFlow RegimesFluid DynamicsFluid Flow PropertiesNumerical AnalysisTurbulenceVortex DynamicsWind Tunnels KeywordsTransonic FlowFreestream Mach NumberWind Tunnel TestsAircraft WingsLaminar Turbulent TransitionWing RootViscosityBusiness AircraftSweep AngleBombardier Global ExpressDigital Published online22 May 2012