Print Email Facebook Twitter Calculation of the flow around a swept wing, taking into account the effect of the three-dimensional boundary layer. Part II: Wing with laminar boundary layer on the lower surface Title Calculation of the flow around a swept wing, taking into account the effect of the three-dimensional boundary layer. Part II: Wing with laminar boundary layer on the lower surface Author van den Berg, B. Piers, W.J. de Boer, E. Institution National Aerospace Laboratory NLR Date 1977-06-22 Abstract The attached flow around a swept wing has been calcTilated with allowance for the effects of boundary layer and wake. In part I a swept wing was considered with a turbulent boundary layer on both the upper and lower wing surface. The present part of the study deals with the calculation of the flow around the same swept wing with a laminar boundary layer on the larger part of the lower surface. The calculation results have been compared with experimental data. Subject swept wingsincompressible flowboundary layer flowthree-dimensional boundary layerturbulent boundary layerslaminar boundary layers To reference this document use: http://resolver.tudelft.nl/uuid:41243555-e848-4767-9949-4bbe75fd199a Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR-TR 77066 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1977 National Aerospace Laboratory NLR Files PDF NLR_TR_77066_U.pdf 9.43 MB Close viewer /islandora/object/uuid:41243555-e848-4767-9949-4bbe75fd199a/datastream/OBJ/view