Turbulence Study

This data is collected using hot-wire anemometry.<br>A NACA 2412 aerofoil was used in this turbulence study. The standard baseline aerofoil has files beginning with 'aerofoil_nonns', and the aerofoil with negative stiffness inclusions has files beginning with 'aerofoil_ns167' since the elements have a Q ratio of 1.67.<br>All aerofoils were tested at 4 angles of attack (0, 4, 8, 12) and 5 freestream velocities (10, 15, 20, 25, 30). This is in the relevant file name.<br>Calibration data for the hot-wire is included. Use these values to convert from voltage to velocity. Use the morning calibration for the nonns aerofoil and afternoon calibration for the ns167 aerofoil.<br>v1 and v1_m is voltage. <br>For acquiring data, Step_2_acquisition.m was usedFor acquiring data, Step_1_calibration.m was used