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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| Format: | Article |
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Aeronautical and Astronautical Society of the Republic of China
2021
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| Online Access: | http://psasir.upm.edu.my/id/eprint/94388/ https://www.airitilibrary.com/Publication/alDetailedMesh?DocID=P20140627004-202106-202102080001-202102080001-143-153 |
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