COMPUTATIONAL STUDY OF FLOW CHARACTERISTICS OVER HIGH LIFT AIRFOIL AT VARIOUS ANGLES OF ATTACK

A numerical simulation aiming to study and investigate flow behavior over a high lift low speed airfoil type AG-16 at various angles of attack ranging from 0 degree to 15 degree and constant Reynolds number “39,709” was performed. Computational fluid dynamic CFD technique was applied to study the...

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Bibliographic Details
Main Authors: Ali H. Mutaib, Amjed AL-Khateeb, Mohammed K. Khashan, Furkan Kamil
Format: Article
Language:English
Published: Zibeline International 2019-01-01
Series:Journal of Mechanical Engineering Research and Developments
Subjects:
Online Access:https://jmerd.org.my/Paper/Vol.42,No.1(2019)/90-95.pdf

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