%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %%%%%% %%%%%% %%%%%% Turbulent Channel Flow with wall-normal rotation %%%%%% %%%%%% %%%%%% %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %%%%%% %%%%%% %%%%%% Supported by the German Science Foundation (DFG) %%%%%% %%%%%% %%%%%% %%%%%% 2006 - 2009 %%%%%% %%%%%% %%%%%% %%%%%% %%%%%% %%%%%% Chair of Fluid Dynamics %%%%%% %%%%%% %%%%%% %%%%%% Department of Mechanical Engineering, %%%%%% %%%%%% Technische Unversitaet Darmstadt, %%%%%% %%%%%% Otto-Berndt-Str. 2, 64287 Darmstadt, Germany %%%%%% %%%%%% %%%%%% %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %%%%%% %%%%%% %%%%%% <<< CAUTION >>> %%%%%% %%%%%% %%%%%% %%%%%% All rights are reserved by the Chair of Fluid Dynamics. %%%%%% %%%%%% No part of the data described herein may be represented %%%%%% %%%%%% without reference. The data base may be used without %%%%%% %%%%%% notification to the author's laboratory. %%%%%% %%%%%% %%%%%% %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% %% %% REFERENCES: %% %% Mehdizadeh A., Oberlack M., (2010): %% %% "Analytical and numerical investigations of laminar and %% %% turbulent Poiseuille-Ekman flow at different rotation rates", %% %% Physics of Fluids, 22, 105104, doi:10.1063/1.3488039 %% %% %% %% %% %% Nomenclature: %% %% Re_tau = u_tau0x*h /nu : Reynolds number %% %% Ro = 2Omega*h / u_tau0x : Rotation number %% %% U = streamwise mean velocity %% %% W = spanwise mean velocity %% %% u_taux= mean friction velocity in the streamwise direction %% %% u_tauz= mean friction velocity in the spanwise direction %% %% h = Channel half height %% %% omega= system rotation rate %% %% x, y, z = streamwise, wall-normal and spanwise directions %% %% + = normalized by wall units, i.e. u_tau0 (friction velocity %% %% for non-rotating case) %% %% %% %% %% %% BOX SIZE (x,y,z): 4pi|2|2pi %% %% MESH NUMBER (x,y,z): 128|129|128 %% %% FLOW CONDITIONS: u_tau0x = 0.0027 %% %% u_tau0z = 0 %% %% Re_tau = 180 %% %% Ro = 0.0 %% %% %% %% NUMERICAL METHOD: %% %% Lundbladh, D. Henningson and A. Johanson, "An Efficient %% %% Spectral Integration Method for the Solution of the %% %% Navier-Stokes Equations", Aeronautical Research Institute of %% %% Sweden, Bromma, 1992 %% %% %% %% Data file created: May 10, 2017 %% %%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %% x2/h U+ W+ uu+ uv+ uw+ vv+ vw+ ww+ %%-------------------------------------------------------------------------------------------------------- 1.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.00000000 0.99969882 0.05484934 -0.00007490 0.00040987 0.00000000 0.00000064 0.00000000 0.00000000 0.00012918 0.99879546 0.21926486 -0.00030004 0.00653923 0.00000825 0.00001068 0.00000000 0.00000000 0.00198027 0.99729046 0.49284076 -0.00007490 0.03298181 0.00009858 0.00005109 0.00000462 -0.00000008 0.00939212 0.99518472 0.87483141 -0.00030004 0.10377161 0.00056459 0.00014638 0.00004100 -0.00000082 0.02714816 0.99247953 1.36390872 -0.00067478 0.25183307 0.00219105 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