Investigation of the vortical flow around a reverse delta wing

A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta...

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Bibliographic Details
Main Authors:	Altaf, Afaq, Omar, Ashraf Ali E., Asrar, Waqar, Ludin@Jamaluddin, Hani
Format:	Conference or Workshop Item
Language:	English
Published:	2011
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/1/paper_4.pdf

id	iium-2364
recordtype	eprints
spelling	iium-23642011-11-21T03:55:03Z http://irep.iium.edu.my/2364/ Investigation of the vortical flow around a reverse delta wing Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar Ludin@Jamaluddin, Hani TL500 Aeronautics A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing. 2011-05 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/2364/1/paper_4.pdf Altaf, Afaq and Omar, Ashraf Ali E. and Asrar, Waqar and Ludin@Jamaluddin, Hani (2011) Investigation of the vortical flow around a reverse delta wing. In: International Conference on Mechanical, Automotive and Aerospace Engineering 2011 (ICMAAE11) , 17-19 May 2011, Legend Hotel, Kuala Lumpur . http://www.iium.edu.my/icmaae/2011/
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English
topic	TL500 Aeronautics
spellingShingle	TL500 Aeronautics Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar Ludin@Jamaluddin, Hani Investigation of the vortical flow around a reverse delta wing
description	A six component force balance was used to obtain the CL for a reverse delta wing and a delta wing for comparison purposes. A simulation of the streamlines, velocity vectors and surface pressure contours was carried out using CFD software to show the characteristics of the flow over a reverse delta wing.
format	Conference or Workshop Item
author	Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar Ludin@Jamaluddin, Hani
author_facet	Altaf, Afaq Omar, Ashraf Ali E. Asrar, Waqar Ludin@Jamaluddin, Hani
author_sort	Altaf, Afaq
title	Investigation of the vortical flow around a reverse delta wing
title_short	Investigation of the vortical flow around a reverse delta wing
title_full	Investigation of the vortical flow around a reverse delta wing
title_fullStr	Investigation of the vortical flow around a reverse delta wing
title_full_unstemmed	Investigation of the vortical flow around a reverse delta wing
title_sort	investigation of the vortical flow around a reverse delta wing
publishDate	2011
url	http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/ http://irep.iium.edu.my/2364/1/paper_4.pdf
first_indexed	2023-09-18T20:09:57Z
last_indexed	2023-09-18T20:09:57Z
_version_	1777407411208847360

Investigation of the vortical flow around a reverse delta wing

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