Numerical study of effect of spoiler configuration on
wake vortex alleviation

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Numerical study of effect of spoiler configuration on wake vortex alleviation

A numerical investigation was undertaken to evaluate the capabilities of differential spoiler setting (DSS) in modifying the span-wise wing load and reducing hazard of wake vortices imposed on a following aircraft. Numerical simulations were carried out on a scaled, half-model aircraft under high l...

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Bibliographic Details
Main Authors:	Ludin@Jamaluddin, Hani, Omar, Ashraf Ali, Asrar, Waqar
Format:	Article
Language:	English English
Published:	American Society of Civil Engineers 2015
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/44185/ http://irep.iium.edu.my/44185/1/ASENG-633_p1.pdf http://irep.iium.edu.my/44185/2/Hani-_ASCE_J_Aero-May_2015.docx

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