Print Email Facebook Twitter Potential flow calculations to support two-dimensional wind tunnel tests on high-lift devices Title Potential flow calculations to support two-dimensional wind tunnel tests on high-lift devices Author Labrujere, T.E. Schipholt, G.J. de Vries, O. Institution National Aerospace Laboratory NLR Date 1972-06-05 Abstract The applicability of potential flow calculations for developing high-lift devices, is evaluated by comparing calculated pressure distributions over wing sections with trailing and leading edge high-lift devices, and experimental results, obtained during routine wind tunnel tests. To reference this document use: http://resolver.tudelft.nl/uuid:0e3c602e-e5f2-461c-b754-083be5acba70 Publisher Nationaal Lucht- en Ruimtevaartlaboratorium Access restriction Campus only Source NLR MP 72016 U Part of collection Aerospace Engineering Reports Document type report Rights (c) 1972 National Aerospace Laboratory NLR Files PDF 72016.pdf 13.34 MB Close viewer /islandora/object/uuid:0e3c602e-e5f2-461c-b754-083be5acba70/datastream/OBJ/view