Wing is one of the most important component for any aircraft. The main purpose of wing is to provide a lift force that can gets the airplane off the ground. Its also raised any airplane to an efficient and safe cruising altitude. In addition, it lets the airplane to maneuver and allows a safe landing. Therefore in the design process of an aircraft it is necessary to investigates the forces acting on the wing in order to obtain one which suits the aircraft operational requirements. Wing is actually made up of aerofoil section. Many types of wing are available which comes in various geometrical shapes. This thesis concerns with wings that operates in subsonic flow.