Numerical study of wind-tunnel wall effects on lift and drag characteristics of NACA 0012 airfoil

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Numerical study of wind-tunnel wall effects on lift and drag characteristics of NACA 0012 airfoil

Possible interference effects of the wind tunnel walls play an important role especially for measurements in closed-wall test sections. In this study, a numerical analysis of two-dimensional subsonic flow over a NACA 0012 airfoil at different computational domain heights, angles of attack from 0o to...

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Bibliographic Details
Main Authors:	Abobaker, Mostafa, M. Elfaghi, Abdulhafid, Addeep, Sogair
Format:	Article
Language:	English
Published:	Akademia Baru Publishing 2020
Subjects:	TL500-777 Aeronautics. Aeronautical engineering
Online Access:	http://eprints.uthm.edu.my/6193/ http://eprints.uthm.edu.my/6193/1/AJ%202020%20%28809%29.pdf

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