Aerodynamics investigation of delta wing at low Reynold’s
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Aerodynamics investigation of delta wing at low Reynold’s number

A numerical simulation has been carried out to investigate the aerodynamics of an oscillating delta wing and to evaluate the flow structure over the leading edge at different low Reynolds numbers. The numerical results of the coefficient of lift (CL) vs angle of attack are validated with the experi...

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Bibliographic Details
Main Authors:	Hamizi, Ilya Bashiera, Khan, Sher Afghan
Format:	Article
Language:	English English
Published:	Penerbit Akademia Baru 2019
Subjects:	TJ Mechanical engineering and machinery TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/70862/ http://irep.iium.edu.my/70862/1/70862_Aerodynamics%20Investigation%20of%20Delta%20Wing.pdf http://irep.iium.edu.my/70862/7/70862_Aerodynamics%20investigation%20of%20delta%20wing_SCOPUS.pdf

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