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_Re1M_xc40 HW diameter [micron]: 2.5 HW length [mm]: 0.7 HW length in viscous units [-]: 58 HW Overheat ratio [%]: 80 sampling freq. [kHz]: 60 analog filter [kHz]: 30 Temperature [C]: 21.43 atm. pressure [Pa]: 102130 kin. viscosity [m^2/s]: 1.5068e-05 Downstream position (x/c from leading edge) [-]: 0.4 Reynolds Number based on chord (Re_c): 1000000 Angle of attack (pos) [degrees]: 8 Freestream vel. [m/s]: 43.6038 Friction velocity [m/s]: 1.6811 Viscous length scale [m]: 8.9633e-06 Calculated values: Displacement thickness, d1 [m]: 0.00091313 Momentum-loss thickness, d2 [m]: 0.00057819 Boundary layer thickness (d99) [m]: 0.0041714 Shape Factor (H_12): 1.579 Re_theta: 1673 Re_tau: 465 Beta: 0.75407 y [m] U [m/s] urms [m/s] 0.00012757 17.32274258 8.67656702 0.00026371 22.29525803 9.14718151 0.00042005 24.69708361 8.56272313 0.00059795 26.38827210 8.39416423 0.00080198 27.98847042 8.39619004 0.00103363 29.65787334 8.40841088 0.00129767 31.33849261 8.16288570 0.00159936 33.08153495 7.80369196 0.00194282 34.94239621 7.21053814 0.00233593 36.86151742 6.30116425 0.00278279 38.85639355 5.09078635 0.00329377 40.84508909 3.56125377 0.00387578 42.65323710 1.84637952 0.00453900 43.80756536 0.53993471 0.00529677 44.17180237 0.12603027 0.00616025 44.15721112 0.05809405 0.00714556 44.06825741 0.03893617 0.00826995 43.99719807 0.03357633 0.00955185 43.93009545 0.03104487