Effect of Micro-Slats on Airfoil Lift and Stall Behavior

This dataset supports the research study “Effect of Micro-Slats on Airfoil Lift and Stall Behavior.” It contains the underlying computational and experimental data used to evaluate passive leading-edge micro-slat configurations on a NACA 2412 airfoil, including XFOIL simulation outputs, Python-based parametric optimization results, wind-tunnel measurements, lift and stall data, and geometry parameters for the tested configurations. The dataset supports comparisons between the baseline airfoil and micro-slat designs across multiple angles of attack and Reynolds numbers.