Print Email Facebook Twitter Approximate method for determining the potential flow about an arbitrary aerofoil section in a two-dimensional finite stream with particular reference to large stream deflections Title Approximate method for determining the potential flow about an arbitrary aerofoil section in a two-dimensional finite stream with particular reference to large stream deflections Author Gould, D.G. Institution National Research Council Canada, National Aeronautical Establishment, Flight Research Date 1959-08-31 Abstract The flow about and on the surface of an aerofoil section in a finite stream and that about and on the surface of the same aerofoil section in an infinite symmetrical cascade are compared. It is shown that, for most cases of practical interest, the differences are small for stream deflection angles up to 90 degrees. Thus, the approximate flow about an arbitrary aerofoil section in a two-dimensional finite stream may be obtained by using the methode existing for the determination of the flow about an arbitrary section in a cascade. The procedure, as applied to the finite stream approximation, is given using the interference method of cascade theory. To reference this document use: http://resolver.tudelft.nl/uuid:e4a3904c-7f6b-47ef-90c2-172bafbfca41 Publisher National Research Council Canada Access restriction Campus only Source National Research Council Aeronautical Report LR 260 Part of collection Aerospace Engineering Reports Document type report Rights (c) 1959 National Research Council Canada Files PDF LR-260.pdf 5.46 MB Close viewer /islandora/object/uuid:e4a3904c-7f6b-47ef-90c2-172bafbfca41/datastream/OBJ/view