%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%%% %%%%%% %%%%%% %%%%%% 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|6pi %% %% MESH NUMBER (x,y,z): 128|129|384 %% %% FLOW CONDITIONS: u_taux = 0.0012 %% %% u_tauz = 0.0015 %% %% Re_tau = 180 %% %% Ro = 0.091 %% %% %% %% 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 0.01235438 0.01879489 0.00002753 0.00000000 0.00024876 0.00000000 0.00000000 0.00005171 0.99879546 0.04931143 0.07516806 0.00042954 0.00000000 0.00397686 0.00000000 0.00000083 0.00082993 0.99729046 0.11055456 0.16908313 0.00212232 0.00000331 0.02007934 0.00000000 0.00000826 0.00418032 0.99518473 0.19556038 0.30047060 0.00649085 0.00002066 0.06322066 0.00000248 0.00004545 0.01312320 0.99247953 0.30359972 0.46920335 0.01522308 0.00008099 0.15356446 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