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_AoA05_Re400k_xc75 HW diameter [micron]: 2.5 HW length [mm]: 0.7 HW length in viscous units [-]: 20 HW Overheat ratio [%]: 80 sampling freq. [kHz]: 60 analog filter [kHz]: 30 Temperature [C]: 20.97 atm. pressure [Pa]: 99447 kin. viscosity [m^2/s]: 1.5432e-05 Downstream position (x/c from leading edge) [-]: 0.75 Reynolds Number based on chord (Re_c): 400000 Angle of attack (pos) [degrees]: 5 Freestream vel. [m/s]: 14.7416 Friction velocity [m/s]: 0.52401 Viscous length scale [m]: 2.945e-05 Calculated values: Displacement thickness, d1 [m]: 0.0028968 Momentum-loss thickness, d2 [m]: 0.0016958 Boundary layer thickness (d99) [m]: 0.010917 Shape Factor (H_12): 1.708 Re_theta: 1620 Re_tau: 371 Beta: 2.8176 y [m] U [m/s] urms [m/s] 0.00014662 2.58207198 1.04043719 0.00020363 3.42067456 1.62375134 0.00026064 4.07440602 1.95917768 0.00031791 4.59603302 2.12738020 0.00037492 5.00469402 2.19027542 0.00043193 5.35218891 2.17074686 0.00048990 5.63134778 2.15711812 0.00057506 5.97751493 2.12620771 0.00066119 6.22668102 2.05168485 0.00074609 6.44343067 2.01339590 0.00083222 6.61826560 1.98067177 0.00091835 6.78001659 1.96430807 0.00100351 6.93676028 1.91969238 0.00115805 7.15069059 1.87663569 0.00133223 7.35200508 1.86154859 0.00152825 7.57617665 1.84885399 0.00175024 7.82953023 1.83002358 0.00200011 8.08395227 1.86243445 0.00228226 8.37135244 1.87445654 0.00260178 8.66603021 1.88443210 0.00296058 8.98338849 1.89209751 0.00336622 9.36990135 1.89130249 0.00382475 9.79465197 1.89301034 0.00434125 10.23508769 1.87561433 0.00492423 10.79779526 1.80861667 0.00558291 11.34249357 1.70582569 0.00632551 11.98356721 1.54587146 0.00716372 12.60932000 1.34003567 0.00810963 13.32000148 1.04960143 0.00917684 14.02048887 0.62754363 0.01038209 14.51932465 0.23187018 0.01174216 14.70952964 0.05070115 0.01327613 14.72848610 0.01327491 0.01500736 14.69251442 0.00512918 0.01696154 14.68997802 0.00224889 0.01916683 14.67120247 0.00113202 0.02165619 14.65011698 0.00062134 0.02446506 14.63756162 0.00039195 0.02763371 14.60223422 0.00028764 0.03121115 14.58729187 0.00022990 0.03524835 14.55579466 0.00020174 0.03980398 14.52310249 0.00018356