Volume 45, Issue 1 No AccessInvestigation of a Half-Model High-Lift Configuration in a Wind TunnelPeter EliassonPeter Eliasson FOI, Swedish Defence Research Agency, 164 90 Stockholm, SwedenSearch for more papers by this authorPublished Online:22 May 2012https://doi.org/10.2514/1.34054SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous article Next article FiguresReferencesRelatedDetailsSee PDF for referencesCited bySemi-span wind tunnel testing without conventional peniche8 November 2017 | Experiments in Fluids, Vol. 58, No. 12Assessment of high-order finite volume methods on unstructured meshes for RANS solutions of aeronautical configurationsComputers & Fluids, Vol. 146Simulation of a Variety of Wings Using a Reynolds Stress ModelK. B. Thompson and H. A. Hassan26 February 2015 | Journal of Aircraft, Vol. 52, No. 5Results from the Second AIAA CFD High-Lift Prediction Workshop Using EdgePeter Eliasson and Shia-Hui Peng10 September 2014 | Journal of Aircraft, Vol. 52, No. 4Numerical Investigations of the High-Lift Configuration with MFlow SolverJiangtao Chen, Yaobing Zhang, Naichun Zhou and Youqi Deng10 April 2015 | Journal of Aircraft, Vol. 52, No. 4Numerical Accuracy in RANS Computations of High-Lift Multi-element Airfoil and Aicraft ConfigurationsDimitrios Drikakis, Panayiotis Tsoutsanis and Antonis F. Antoniadis3 January 2015Numerical Investigation of Wall Mounting Effects in Semi-Span Wind-Tunnel TestsMohamed Bouriga, François Morency and Julien Weiss2 January 2015Results from the 2nd AIAA CFD High Lift Prediction Workshop using EdgePeter Eliasson10 January 2014A short history of the European Transonic Wind Tunnel ETWProgress in Aerospace Sciences, Vol. 47, No. 5Influence of Transition on High-Lift Prediction with the NASA Trap Wing ModelPeter Eliasson, Ardeshir Hanifi and Shia-Hui Peng4 July 2012Improving the Prediction for the NASA High-Lift Trap Wing ModelPeter Eliasson, Shia-Hui Peng and Ardeshir Hanifi14 June 20125-Degree-of-Freedom Dynamic Rig for Wind Tunnel Tests of Aerospace VehiclesArpita Sen, Niteen Bhange, Pankaj Wahi and Ajoy Ghosh14 June 2012Design of a High Lift System with a Leading Edge Droop NoseAdam Jirasek and Olivier Amoignon14 June 2012Application of a Line-Implicit Scheme on Stretched Unstructured GridsPeter Eliasson, Jan Nordström and Per Weinerfelt15 June 2012Geometrical Installation and Deformation Effects in High-Lift Flows J. W. van der Burg , H. Freiherr von Geyr , R. Heinrich , P. Eliasson , T. Delille and J. Krier 2 May 2012 | AIAA Journal, Vol. 47, No. 1 What's Popular Volume 45, Number 1January 2008 Crossmark TopicsAerodynamic PerformanceAerodynamicsAerospace SciencesBoundary LayersComputational Fluid DynamicsFinite Element MethodFlow RegimesFluid DynamicsFluid MechanicsMesh GenerationSkin FrictionVortex DynamicsWind Tunnels KeywordsLow Speed Wind TunnelLift CoefficientTotal Variation DiminishingFuselage ConfigurationsUnstructured GridFreestream Mach NumberReynolds Averaged Navier StokesStatic PressureLaminar Turbulent TransitionFlow ConditionsPDF Published online22 May 2012