The current investigation is performing the computational analalysis by applying the Magnus effect to an airplane wing. Magnus pressures can be used to raise CD and CL values, and the scope and focus of the Magnus effect survey in aerospace engineering are both steadily expanding globally. Despite sufficient lift force being created, several experiments failed due to the considerable drag caused by large cylinders. The Magnus effect's one flaw is that it can be used on symmetrical bodies like cylinders, in this case, the cambered airfoil. By preserving the revolving cylinder flow over an airfoil profile, the current work provides an alternative approach to use. The Flo-lapse method is used to start the project. It involves using a cambered airfoil, analyzing its aerodynamic properties, and performing performance by using the Magnus effect. A faster circumferential speed may lead to better CD and CL values and an earlier delay in the development of the boundary layer. ANSYS (fluent) software is used to compare the aerodynamic differences between the rectangular wing with and without a cylinder.