% Turbulent boundary layer measurement in the MTL wind tunnel,
% KTH July-August 2008, Version 1.5, 18-Dec-2013 
% 
% The experiment is described in detail in: Ramis Orlu (2009) 
% Experimental studies in jet flows and 
% zero pressure-gradient turbulent boundary layers, PhD thesis, 
% KTH Mechanics, Stockholm, Sweden 
% http://www.mech.kth.se/mech/info_defense.jsp?DefenseID=560 
% Reference: Orlu and Schlatter (2013) Comparison of 
% experiments and simulations for zero pressure gradient 
% turbulent boundary layers at moderate Reynolds numbers. 
% Exp. Fluids, 43:1547; http://dx.doi.org/10.1007/s00348-013-1547-x  
% (Note that integral quantities are computed by following the scheme 
% outlined in Schlatter and Orlu [2010, J. Fluid Mech., 659, 116-126]; 
% number of decimal places does not indicate accuracy of data.) 
% 
% Measurements done by: Ramis Orlu, 
% Contact: ramis@mech.kth.se 
% 
% Asociation case number 
% TA1-6=[65 67 66 63]
% TB1-7=[74 75 73 76 70 72 69]
% TC1-3=[78 80 79]
% 
% EXPno  U_inf[m/s]  Re_d2  Re_tau  d99[mm]  d1[mm]  d2[mm]  H_12  c_f*1e3
63 29.92 6334.5 2016.4  27.2250   4.3350   3.2047   1.3527   2.8080 
65 19.94 4348.4 1399.6  27.4789   4.5486   3.3038   1.3768   2.9952 
66 26.41 5661.7 1808.4  27.4458   4.4181   3.2460   1.3611   2.8541 
67 24.99 5382.8 1715.3  27.4029   4.4458   3.2618   1.3630   2.8775 
69 29.97 5751.4 1780.8  24.1373   4.0013   2.9207   1.3700   2.8075 
70 20.06 4025.5 1275.7  25.0135   4.2261   3.0536   1.3840   2.9933 
72 28.08 5374.7 1666.2  24.0248   4.0041   2.9154   1.3735   2.8304 
73 16.78 3466.9 1112.4  25.6057   4.3864   3.1479   1.3934   3.1121 
74 11.53 2312.9 790.2  25.2538   4.3047   3.0563   1.4084   3.4192 
75 12.07 2441.8 828.3  25.4347   4.3293   3.0807   1.4053   3.3761 
76 17.41 3591.3 1153.0  25.6636   4.3669   3.1386   1.3913   3.0834 
78 12.05 2511.6 845.9  25.8205   4.4276   3.1474   1.4067   3.3710 
79 17.13 3600.3 1149.4  25.7633   4.4220   3.1731   1.3936   3.0921 
80 16.68 3520.4 1123.5  25.7956   4.4490   3.1869   1.3960   3.1091