Print Email Facebook Twitter Computations of incompressible turbulent boundary layers on rough surfaces Title Computations of incompressible turbulent boundary layers on rough surfaces Author Chan, Y.Y. Institution National Research Council Canada, National Aerospace Establishment, High Speed Aerodynamics Section Date 1971-05-31 Abstract The extended mixing length formulation for the computation of incompressible turbulent boundary layers has been applied with success to flows over rough surfaces. The roughness effect is introduced into the computation scheme through the boundary conditions by defining a slip velocity at the surface. The method predicts the mean velocity and the turbulent shear stress distributions accurately except for a region near the wall where the flow is influenced locally by the roughness element To reference this document use: http://resolver.tudelft.nl/uuid:b3e125a8-a855-4bd3-a241-68398d0e2274 Publisher National Research Council Canada Access restriction Campus only Source National Research Council Aeronautical Report LR 546 Part of collection Aerospace Engineering Reports Document type report Rights (c)1971 National Research Council Canada Files PDF LR-546.pdf 3.34 MB Close viewer /islandora/object/uuid:b3e125a8-a855-4bd3-a241-68398d0e2274/datastream/OBJ/view