Print Email Facebook Twitter Design of an airfoil leading edge slat using an inverse aerodynamic calculations method Title Design of an airfoil leading edge slat using an inverse aerodynamic calculations method Author van Egmond, J.A. van den Berg, B. Institution National Aerospace Laboratory NLR Date 1984-05-02 To reference this document use: http://resolver.tudelft.nl/uuid:3556e392-0cdb-4825-8a5c-280b9e89c94d Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 84044 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1984 National Aerospace Laboratory NLR Files PDF 84044.pdf 7.71 MB Close viewer /islandora/object/uuid:3556e392-0cdb-4825-8a5c-280b9e89c94d/datastream/OBJ/view