Print Email Facebook Twitter Computation of three-dimensional boundary layer transition and separation on a 65deg swept delta wing at 20deg angle of attack Title Computation of three-dimensional boundary layer transition and separation on a 65deg swept delta wing at 20deg angle of attack Author de Bruin, A.C. Hoeijmakers, H.W.M. Institution National Aeropsace Laboratory NLR Date 1986-11-20 Abstract Laminar and turbulent boundary layer calculations were carried out on the leeward side of a flat sharp-edged delta wing. The prediction of laminar-turbulent boundary layer transition and the prediction of secondary separation are addressed in some detail. To reference this document use: http://resolver.tudelft.nl/uuid:e58976cf-c4ac-4914-a69d-489c16d15522 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 86075 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1986 National Aeropsace Laboratory NLR Files campus only