No Access2D Investigation of the Flow Through a Symmetric Variable Inlet Guide Vane, Part 1: Experimental AnalysisDavid Händel, Sebastian Barthmes, Reinhard Niehuis, Uwe Rockstroh and Lennart LeopoldDavid HändelUniversity of the German Federal Armed ForcesSearch for more papers by this author, Sebastian BarthmesUniversity of the German Federal Armed ForcesSearch for more papers by this author, Reinhard NiehuisUniversity of the German Federal Armed ForcesSearch for more papers by this author, Uwe RockstrohMAN Diesel & Turbo SESearch for more papers by this author and Lennart LeopoldMAN Diesel & Turbo SESearch for more papers by this authorAIAA 2013-3682Session: Compressor IIIPublished Online:12 Jul 2013https://doi.org/10.2514/6.2013-3682SectionsRead Now ToolsAdd to favoritesDownload citationTrack citations ShareShare onFacebookTwitterLinked InRedditEmail About Previous chapter Next chapter FiguresReferencesRelatedDetailsSee PDF for referencesCited byLoss Characterization of Advanced VIGV Configurations With Adjustable Blade Geometry2 November 2021 | Journal of Turbomachinery, Vol. 144, No. 32D Investigation of the Flow Through a Symmetric Variable Inlet Guide Vane, Part 2: Numerical AnalysisSebastian Barthmes, David Händel, Reinhard Niehuis, Christian Wacker and Jan Klausmann12 July 2013 What's Popular 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference July 14 - 17, 2013San Jose, CAhttps://doi.org/10.2514/6.2013-3682 CrossmarkInformationCopyright © 2013 by David Händel[|#3#|], Sebastian Barthmes[|#3#|], Reinhard Niehuis[|#3#|], Uwe Rockstroh, Lennart Leopold. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. TopicsAerodynamicsAeronautical EngineeringAeronauticsBoundary LayersComputational Fluid DynamicsFinite Element MethodFinite Element SoftwareFlow RegimesFluid DynamicsFluid MechanicsPneumaticsTurbulenceVortex DynamicsWind Tunnels KeywordsMach NumbersTurbulent Boundary LayerRadial CompressorsNumerical SimulationCascade Wind TunnelsShear StressJet PropulsionIndustrial ApplicationsStagnation PointStatic PressurePDF Topics Joint Propulsion