Comparative Analysis of Aerodynamic Lift and Drag of Commercially Used Air-foil Incorporated with Co-flow Jet

Abstract

Abstract In this research, a baseline airfoil is modified by incorporating a Co-flow Jet into the airfoil. Co-flow jet is also called zero net mass flux as the same amount of highly pressurized air is injected towards the streamlines of an airfoil from the leading edge and sucks this air without changing the amount in the trailing edge using an air pump. A performance boost is expected for the use of the Co-flow Jet. An airplane’s performance is based on a few parameters such as the coefficient of lift, coefficient of drag, boundary layer separation, and many others. In this research, a comparative analysis is run between a baseline airfoil and a CFJ airfoil. NACA-4412 is chosen as the target airfoil. The research shows how the incorporation of CFJ in an airfoil increases the coefficient of lift (CL) and decreases the coefficient of drag (CD). Thus, it is possible to maintain a better CL/CL ratio by using CFJ. The research also mentions the increase in stall angle due to the use of CFJ. It is a computational analysis performed in the software Ansys. For simplicity, the analysis is limited to two-dimensional analysis. This research may bring a better improvement in the aircraft and aerodynamic sectors. Though the results obtained from the research may not fully be similar to the hypothesis, it has been tried to maintain that the results of the simulation hardly differ from the theoretical analysis.