Numerical simulation of aerofoil with flow injection at the upper surface

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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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Bibliographic Details
Main Authors:	Chua, Bing Liang, Mohammed, Akmal Nizam, Sapit, Azwan, Razali, Mohd Azahari, Hushim, Mohd Faisal, Khalid, Amir, Mohd Yusof, Nurul Farhana
Format:	Article
Language:	English
Published:	Penerbit Akademia Baru 2020
Subjects:	T Technology (General) TJ Mechanical engineering and machinery
Online Access:	http://eprints.uthm.edu.my/6308/ http://eprints.uthm.edu.my/6308/1/AJ%202020%20%28268%29.pdf

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