In this project, it is aimed to mathematically model the laminar separation bubble that occurs in airfoils used in wind turbines and micro unmanned aerial vehicles, especially in low Reynolds number flows. Wind Engineering Aerodynamics Research Laboratory of Erciyes University Energy Systems Engineering is used to create the mathematical model. The experimental results obtained from the wind tunnel here and the numerical studies carried out simultaneously will be correlated with each other and the laminar separation bubble will be modeled.