CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing

Winglets are one of important part of the wing that can reduce the vortex formed at the wing tips and therefore reduce induced drag by partial recovery of the tip vortex energy. Moreover, they increase the effective aspect ratio without actually increasing the wingspan. The geometry of the wingle...

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Main Authors:	Munshi, Adnan, Sulaeman, Erwin, Omar, Norfazzila, Ali, Mohammad Yeakub
Format:	Article
Language:	English English
Published:	Penerbit Akademia Baru 2018
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/64671/ http://irep.iium.edu.my/64671/ http://irep.iium.edu.my/64671/1/64671_CFD%20Analysis%20on%20the%20Effect%20of%20Winglet.pdf http://irep.iium.edu.my/64671/2/64671_CFD%20Analysis%20on%20the%20Effect%20of%20Winglet_SCOPUS.pdf

id	iium-64671
recordtype	eprints
spelling	iium-646712018-07-25T01:33:30Z http://irep.iium.edu.my/64671/ CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing Munshi, Adnan Sulaeman, Erwin Omar, Norfazzila Ali, Mohammad Yeakub TL500 Aeronautics Winglets are one of important part of the wing that can reduce the vortex formed at the wing tips and therefore reduce induced drag by partial recovery of the tip vortex energy. Moreover, they increase the effective aspect ratio without actually increasing the wingspan. The geometry of the winglets plays an important role in their task. In the present research, computation of lift and drag of ONERA M6 wing have been conducted using ANSYS Fluent. The results have been validated with the NASA results. Flow features of the entire wing including winglet were examined at different cant angles of winglets of 30°, 60° and 75° at different angles of attack from 3° to 6°. It is observed that among the cases of this study, wings with winglets produces higher CL/CD ratio than the normal aircraft wing without winglets up to certain degree of angle of attack and by further increasing to higher angle of attack its performance getting diminished. The investigated concept of adaptable angle winglets appears to be a likely substitute for refining the aerodynamic effectiveness of an aircraft. Penerbit Akademia Baru 2018-05-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/64671/1/64671_CFD%20Analysis%20on%20the%20Effect%20of%20Winglet.pdf application/pdf en http://irep.iium.edu.my/64671/2/64671_CFD%20Analysis%20on%20the%20Effect%20of%20Winglet_SCOPUS.pdf Munshi, Adnan and Sulaeman, Erwin and Omar, Norfazzila and Ali, Mohammad Yeakub (2018) CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing. Journal of Advanced Research in Fluid Mechanics and Thermal Sciences, 45 (1). pp. 44-54. ISSN 2289-7879 http://www.akademiabaru.com/doc/ARFMTSV45_N1_P44_54.pdf
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics Munshi, Adnan Sulaeman, Erwin Omar, Norfazzila Ali, Mohammad Yeakub CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
description	Winglets are one of important part of the wing that can reduce the vortex formed at the wing tips and therefore reduce induced drag by partial recovery of the tip vortex energy. Moreover, they increase the effective aspect ratio without actually increasing the wingspan. The geometry of the winglets plays an important role in their task. In the present research, computation of lift and drag of ONERA M6 wing have been conducted using ANSYS Fluent. The results have been validated with the NASA results. Flow features of the entire wing including winglet were examined at different cant angles of winglets of 30°, 60° and 75° at different angles of attack from 3° to 6°. It is observed that among the cases of this study, wings with winglets produces higher CL/CD ratio than the normal aircraft wing without winglets up to certain degree of angle of attack and by further increasing to higher angle of attack its performance getting diminished. The investigated concept of adaptable angle winglets appears to be a likely substitute for refining the aerodynamic effectiveness of an aircraft.
format	Article
author	Munshi, Adnan Sulaeman, Erwin Omar, Norfazzila Ali, Mohammad Yeakub
author_facet	Munshi, Adnan Sulaeman, Erwin Omar, Norfazzila Ali, Mohammad Yeakub
author_sort	Munshi, Adnan
title	CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
title_short	CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
title_full	CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
title_fullStr	CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
title_full_unstemmed	CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing
title_sort	cfd analysis on the effect of winglet cant angle on aerodynamics of onera m6 wing
publisher	Penerbit Akademia Baru
publishDate	2018
url	http://irep.iium.edu.my/64671/ http://irep.iium.edu.my/64671/ http://irep.iium.edu.my/64671/1/64671_CFD%20Analysis%20on%20the%20Effect%20of%20Winglet.pdf http://irep.iium.edu.my/64671/2/64671_CFD%20Analysis%20on%20the%20Effect%20of%20Winglet_SCOPUS.pdf
first_indexed	2023-09-18T21:31:46Z
last_indexed	2023-09-18T21:31:46Z
_version_	1777412558642216960

CFD analysis on the effect of winglet cant angle on aerodynamics of ONERA M6 wing

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