"uuid","repository link","title","author","contributor","publication year","abstract","subject topic","language","publication type","publisher","isbn","issn","patent","patent status","bibliographic note","access restriction","embargo date","faculty","department","research group","programme","project","coordinates" "uuid:a6de02bc-1564-43ab-83b0-8981ccd96191","http://resolver.tudelft.nl/uuid:a6de02bc-1564-43ab-83b0-8981ccd96191","Boundary-layer calculations on the leeward surface of a slender delta wing at incidence","de Bruin, A.C.","","1983","The three dimensional flow field around delta wings with leading-edge vortex flow can be computed with panel methods. However, secondary flow separation may occur on the leeward surface of the wing. The associated free vortex sheet can be modeled in the potential flow calculation method, if the location of the secondary separation is provided by a boundary layer calculation method.","computational fluid dynamics; potential flow; three-dimensional boundary layer; compressible boundary layer; laminar boundary layer; turbulent boundary layer; boundary layer separation; delta wings; pressure distribution; vortex sheets; leading edges; secondary flow; computational grids; computer programs; run time (computers); data storage","en","report","Nationaal Lucht- en Ruimtevaartlaboratorium","","","","","","Campus only","","","","","","",""