Numerical simulation of aerofoil with flow injection at the upper surface
Separation of the boundary layer over an airfoil causes a significant increase in the adverse pressure gradients and the losses of energy resulting in the reduction of the lift force and the increment of drag force. Therefore, delaying and eliminating flow separation is necessary to improve its aero...
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Main Authors: | , , , , , , |
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Format: | Article |
Language: | English |
Published: |
Penerbit Akademia Baru
2020
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Subjects: | |
Online Access: | http://eprints.uthm.edu.my/6308/1/AJ%202020%20%28268%29.pdf http://eprints.uthm.edu.my/6308/ |
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