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Effects of Strong Irregular Roughness on the Turbulent Boundary Layer
Authors:Chelakara S Subramanian  Paul I King  Mark F Reeder  Shichuan Ou  Richard B Rivir
Institution:1. Department of Mechanical and Aerospace Engineering, Florida Institute of Technology, Florida, U.S.A
2. Department of Aeronautics and Astronautics, Air Force Institute of Technology, WPAFB, Ohio, U.S.A
3. Propulsion Directorate, Air Force Research Laboratory, WPAFB, Ohio, U.S.A
Abstract:Some recent studies with irregular roughness suggest that the Nikuradse Nikuradse, J., NACA TM 1292, National Advisory Committee on Aeronautics (1933)] equivalent sand-grain roughness measure gives inconsistent results of the flow characteristics. In situations where the roughness is very strong to stifle or diminish the viscous effects the viscous scaling laws alone will not be very meaningful. The present study aims to find an alternative scaling parameter for such cases. Here, the measured mean and turbulent velocity profiles on a nonuniform roughness surface, simulating a gas turbine blade roughness, are presented. A nonzero wall normal pressure gradient is caused which is believed to contribute to the velocity deficit in the near-wall rough boundary layer velocity profile. The surface pressure variation is also directly influenced by the local roughness. The normal turbulent stresses are increased on the rough surface, the vertical component more than the longitudinal component. A pressure gradient velocity scale (similar to that proposed for adverse pressure gradient boundary layer modeling by Durbin and Belcher Durbin, P.A. and Belcher, S.E., J. Fluid Mech. 238 (1992), 699-722] is defined to capture the pressure effects induced by such roughness on the inner layer properties.
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