Turbulent boundary layer measurements around a NACA 4412 wing profile Details about the experiments can be found in: Mallor, F., Sanmiguel Vila, C., Hajipour, M., Vinuesa, R., Schlatter, P. and Örlü, R. (2025) Experimental characterization of turbulent boundary layers around a NACA 4412 wing profile. Exp. Therm. Fluid Sci. 160:111327. DOI: 10.1016/j.expthermflusci.2024.111327 Contact scientist: Ramis Orlu, ramis.orlu@oslomet.no (Note that number decimal places does not indicate the accuracy of the data.) Date: 02-Dec-2024 orig. case name: HW_AoA08_Re400k_xc75 HW diameter [micron]: 2.5 HW length [mm]: 0.7 HW length in viscous units [-]: 16 HW Overheat ratio [%]: 80 sampling freq. [kHz]: 60 analog filter [kHz]: 30 Temperature [C]: 21.1 atm. pressure [Pa]: 100490 kin. viscosity [m^2/s]: 1.5284e-05 Downstream position (x/c from leading edge) [-]: 0.75 Reynolds Number based on chord (Re_c): 400000 Angle of attack (pos) [degrees]: 8 Freestream vel. [m/s]: 14.2872 Friction velocity [m/s]: 0.41953 Viscous length scale [m]: 3.6431e-05 Calculated values: Displacement thickness, d1 [m]: 0.0038864 Momentum-loss thickness, d2 [m]: 0.0021028 Boundary layer thickness (d99) [m]: 0.012902 Shape Factor (H_12): 1.848 Re_theta: 1966 Re_tau: 354 Beta: 6.4537 y [m] U [m/s] urms [m/s] 0.00017898 2.11478360 0.84835799 0.00020744 2.43029096 1.07437240 0.00023495 2.67178963 1.25490368 0.00026341 2.93936810 1.37562399 0.00029187 3.17193121 1.52009946 0.00032033 3.41271225 1.62363971 0.00034879 3.57801882 1.67577884 0.00037725 3.74087068 1.69438781 0.00037725 3.74254462 1.72502121 0.00043418 4.03512955 1.75324641 0.00049015 4.28176550 1.78417357 0.00054707 4.48092692 1.77779720 0.00060367 4.67184949 1.79177953 0.00066059 4.83275879 1.74513819 0.00071657 4.97301295 1.78329756 0.00080195 5.16844391 1.74394833 0.00088733 5.30640168 1.72542581 0.00097176 5.48886428 1.73180075 0.00105683 5.60845921 1.70859964 0.00114221 5.71512138 1.69719856 0.00122664 5.80958671 1.67730717 0.00139108 6.02888603 1.71112113 0.00157860 6.18515858 1.71896187 0.00179143 6.42736182 1.72223063 0.00203397 6.60821711 1.76976088 0.00231004 6.85900810 1.79096269 0.00262405 7.14253399 1.83656073 0.00298139 7.40587388 1.87758464 0.00338838 7.75724961 1.90511845 0.00385197 8.16587208 1.95552703 0.00437880 8.57842164 1.99334469 0.00497963 9.07799410 1.98636513 0.00566237 9.65951145 1.94645803 0.00643934 10.32404708 1.82071673 0.00732446 11.01050096 1.72450617 0.00833102 11.82855174 1.50974451 0.00947766 12.64444681 1.17551219 0.01078241 13.45745595 0.71472060 0.01226710 14.06804787 0.24091035 0.01395766 14.27112060 0.04214080 0.01588190 14.26217542 0.01086523 0.01807115 14.21367646 0.00414503 0.02056366 14.18073008 0.00180572 0.02340054 14.15647534 0.00087949 0.02662954 14.13976940 0.00049682 0.03030474 14.12505388 0.00031720 0.03448843 14.09225166 0.00023202 0.03924988 14.07025116 0.00019158 0.04466907 14.04723579 0.00017287 0.05083741 14.02018818 0.00015184