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_AoA11_Re1M_xc60 HW diameter [micron]: 2.5 HW length [mm]: 0.7 HW length in viscous units [-]: 34 HW Overheat ratio [%]: 80 sampling freq. [kHz]: 60 analog filter [kHz]: 30 Temperature [C]: 21.43 atm. pressure [Pa]: 102470 kin. viscosity [m^2/s]: 1.5018e-05 Downstream position (x/c from leading edge) [-]: 0.6 Reynolds Number based on chord (Re_c): 1000000 Angle of attack (pos) [degrees]: 11 Freestream vel. [m/s]: 38.0917 Friction velocity [m/s]: 0.96428 Viscous length scale [m]: 1.5575e-05 Calculated values: Displacement thickness, d1 [m]: 0.00283 Momentum-loss thickness, d2 [m]: 0.001551 Boundary layer thickness (d99) [m]: 0.0090841 Shape Factor (H_12): 1.825 Re_theta: 3934 Re_tau: 583 Beta: 7.0028 y [m] U [m/s] urms [m/s] 0.00011094 7.92326596 5.83773077 0.00014762 9.08313145 6.58705847 0.00018462 10.05031538 7.20221647 0.00022162 10.81006836 7.45004847 0.00030257 12.00046315 7.54308931 0.00039618 12.89716802 7.48212753 0.00050369 13.67204400 7.45697780 0.00062892 14.37243791 7.54768238 0.00077312 15.04925050 7.69357057 0.00093946 15.73656868 7.98022060 0.00113300 16.46023403 8.27041480 0.00135530 17.16313704 8.58171616 0.00161303 17.95561203 8.87887343 0.00191218 18.88345097 9.30858721 0.00225625 19.87249372 9.52449214 0.00265533 21.14978865 9.82906464 0.00311639 22.51885849 10.02897374 0.00364892 24.22430183 9.94333712 0.00426494 26.07016498 9.69830085 0.00497741 28.27614193 8.92176337 0.00580087 30.60120555 7.71629635 0.00675336 33.12554073 5.99423443 0.00785447 35.75171551 3.57799554 0.00912825 37.78118332 0.97131000 0.01059998 38.30173983 0.14181019 0.01230225 38.26888645 0.05965375 0.01427078 38.21713538 0.04022721 0.01654574 38.14850205 0.03325472 0.01917646 38.07516379 0.03033605 0.02221860 38.00796795 0.02711907 0.02573571 37.91103543 0.02633261 0.02980243 37.81137066 0.02395759 0.03450478 37.72748546 0.02417340