The effects of reynolds number on flow separation of Naca Aerofoil

The effects of reynolds number on flow separation of Naca Aerofoil

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The purpose of this study is to investigate the flow separation above UTM 2D Airfoil at three different Reynolds numbers which are 1 × 106, 1.5 × 106 and 2 × 106 using pressure distribution method and flow visualization. The experiment was conducted in UTM-LST (Low Speed Tunnel). The pressure distri...

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Bibliographic Details
Main Authors:	Abdul Hakim, Muhammad Syahmi, Ab. Wahid, Mastura, Othman, Norazila, Mat, Shabudin, Mansor, Shuhaimi, Dahalan, Md. Nizam, Wan Ali, Wan Khairuddin
Format:	Article
Language:	English
Published:	Penerbit Akademia Baru 2018
Subjects:	TJ Mechanical engineering and machinery
Online Access:	http://eprints.utm.my/85325/1/MuhammadSyahmi2018_TheEffectsofReynoldsNumberonFlowSeparation.pdf

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