Studi Numerik dan Eksperimen Aerodinamika Airfoil NACA 24112

This study aims to investigate experimentally and numerically the characteristics of the NACA 24112 airfoil. This study focuses on investigations of lift coefficient (CL), drag coefficient (CD), and CL / CD ratio and pressure, including flow visualisation around the airfoil. The study was conducted at an angle of attack ranging to -15°-20° and various Mach number at 0.0728 and 0.0809. The experimental test used a test specimen with a span...