Print Email Facebook Twitter Correction for wall-interference by means of a measured-boundary-condition method Title Correction for wall-interference by means of a measured-boundary-condition method Author Labrujere, T.E. Institution National Aerospace Laboratory NLR Date 1984-11-21 Abstract A description is given of a method for the determination of global corrections for wall interference in both solid- and ventilated wall windtunnels, 2D as well as 3D. The method is based on the assumption that the flow velocity is known at a control surface surrounding the model and that the main part of the flow field may be considered irrotational and subsonic. The applicability is illustrated by means of some numerical test cases. Subject windtunnel wallstwo dimensional flowthree dimensional flowirrotational flowsubsonic flowgreen functionGoethert rulecorrectionaerodynamic interferencevelocity distributionslotted windtunnelsnumerical analysisairfoilslift devices To reference this document use: http://resolver.tudelft.nl/uuid:fcaf61d6-ed6f-43b1-a0fe-731951fa23ab Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 84114 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1984 National Aerospace Laboratory NLR Files PDF NLR_TR_84114_U.pdf 14.01 MB Close viewer /islandora/object/uuid:fcaf61d6-ed6f-43b1-a0fe-731951fa23ab/datastream/OBJ/view