Numerical analysis of leading edge cylinder aerofoil on Selig S1223 for moving surface boundary control

• Main Authors: Mohammad Ali, Hidayatullah, Mohd Rafie, Azmin Shakrine, Md Ali, Syaril Azrad
• Format: Article
• Published: Aeronautical and Astronautical Society of the Republic of China 2021
• Online Access: http://psasir.upm.edu.my/id/eprint/94388/; https://www.airitilibrary.com/Publication/alDetailedMesh?DocID=P20140627004-202106-202102080001-202102080001-143-153

The Leading Edge Cylinder Aerofoil has resulted in an outpour of research studies for almost a century till date but fewer attempt has focused on the embedment of a cylinder with undercambered aerofoil. This research was aimed to ascertain whether the concept could enhance the intended aerofoil’s ae...