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Lift Enhancement over an Aerofoil Surface by Circulation Control


Hariramakrishnan , SNS College of Technology; Manjula. K, SNS College of Technology; Marichamy. K, SNS College of Technology; Dhineshkumar. A, SNS College of Technology; Saran Raj. G, SNS College of Technology


unsymmetrical aerofoil, aerofoil NACA 2711, design of modified aerofoil, 2D unsymmetrical aerofoil, angle of attacks, different altitude


The lift generation in the wing is based on the many principles. One the main source is by circulation effect over the wing surface. This process is achieved by adopting two modifications over the wing surface. This process can be incorporated to the any wing surface of the aircraft. To ensure the lift generation, the aerofoil NACA 2711 base model has been analysis and design of modified aerofoil has been analysis through ANSYS. Two modified even can be compared with the base line aerofoil and stated which one is producing the better effect over the wing surface with different angle of attack and different altitude. For this process, the 2D unsymmetrical aerofoil to be selected and analysis should be made out of it.

Other Details

Paper ID: IJSRDV5I20169
Published in: Volume : 5, Issue : 2
Publication Date: 01/05/2017
Page(s): 518-521

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