Print Email Facebook Twitter Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds Title Comparison of boundary layer trips of disk and grit types on airfoil performance at transonic speeds Author Chan, Y.Y. Institution National Research Council Canada, National Aeronautical Establishment Date 1988-12-31 Abstract The effects on aerodynamic performance of a supercritical airfoil applying disk or grit tripping for boundary layer transition has been investigated for a typical supercritical airfoil at transonic speeds. It is observed that by allowing the laminar flow passing through the space between the disks, transition takes place a short distance downstream from the disk trip line. The boundary layer developed downstream from the disk trip is therefore slightly thinner than that from a grit trip. The vortex generating mechanism of the disks may also enhance this development. This small difference has negligible effect on aerodynamics of the airfoil at low lift. However, at high lift, the difference in boundary layer developments is amplified by the strong shock wave and the severe adverse pressure gradient. The thinner and more energetic boundary layer induced by the disk trip will yield higher lift, lower drag and higher trailing edge pressure. To reference this document use: http://resolver.tudelft.nl/uuid:ad9ea724-db22-4b00-a183-8e3137a49692 Publisher National Research Council Canada Access restriction Campus only Source National Aeronautical Establishment, Aeronautical Note NAE-AN-56, NRC no 29908 Part of collection Aerospace Engineering Reports Document type report Rights (c) 1988 National Research Council Canada Files PDF NAE-AN-56.pdf 4.78 MB Close viewer /islandora/object/uuid:ad9ea724-db22-4b00-a183-8e3137a49692/datastream/OBJ/view