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

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

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...

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Bibliographic Details
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/

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