Computational Procedure to Investigate the Boundary Layer Growth Parameters on Conventional Aerfoil

This work includes computational procedure to solve Navier-Stocks equation of viscous flow over 4415 airfoil. Three computer programs have been established to predict the boundary layer growth parameters over the selected airfoil at different angles of attack and different Reynolds numbers. The results have demonstrated that the procedure is capable to predict the boundary layer parameters and position of the separation point is determined correctly at each tested angle of attack.