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...
Main Authors: | , , , |
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Format: | Article |
Language: | English |
Published: |
Zibeline International
2019-01-01
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Series: | Journal of Mechanical Engineering Research and Developments |
Subjects: | |
Online Access: | https://jmerd.org.my/Paper/Vol.42,No.1(2019)/90-95.pdf |