Aeroelastic wind tunnel test of a highly flexible wing at low Reynolds numbers

In this dataset, experimental data from an aeroelastic wind tunnel test of a highly flexible wing are presented. A more in-depth description of the experiment is to be provided in a research article. The data are organized into archives by angle of attack, within each archive the names of the files denote the flow speed, and whether the wing was impacted or not. Each file has 6 columns, with their meaning provided below: Timestamp in h:m:s format Timestamp miliseconds Leading edge out-of-plane accelerometer voltage, the sensitivity of the accelerometer after amplification is 0.02 (m/s^2)/mV Mid-chord in-plane accelerometer voltage, the sensitivity of the accelerometer after amplification is 0.02 (m/s^2)/mV Trailing edge out-of-plane accelerometer voltage, the sensitivity of the accelerometer after amplification is 0.02 (m/s^2)/mV Laser triangulator voltage, measuring out-of-plane displacement, the distance in meters can be calculated by using equation ((voltage in mV)/250 - 4)/32