Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed

It is well known that a big aviation market in the world is air transport of passengers and goods and buoyant aerial vehicles are one of the potential candidates for such applications. Aerodynamic and stability characteristics of such vehicles are critical issues of design and any new such design sh...

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Main Authors:	UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf A., Sulaeman, Erwin, Syed Mohamed Ali, Jaffar
Format:	Conference or Workshop Item
Language:	English English English
Published:	2015
Subjects:	TL Motor vehicles. Aeronautics. Astronautics
Online Access:	http://irep.iium.edu.my/46469/ http://irep.iium.edu.my/46469/ http://irep.iium.edu.my/46469/1/AeroHybrid_Buoyant.pdf http://irep.iium.edu.my/46469/4/62nd_CASI_Aeronautics_Conference_and_AGM_3rd_GARDN_Conference_Programme.pdf http://irep.iium.edu.my/46469/5/62nd_CASI_abstract.pdf

id	iium-46469
recordtype	eprints
spelling	iium-464692016-01-27T00:39:51Z http://irep.iium.edu.my/46469/ Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed UlHaque, Anwar Asrar, Waqar Omar, Ashraf A. Sulaeman, Erwin Syed Mohamed Ali, Jaffar TL Motor vehicles. Aeronautics. Astronautics It is well known that a big aviation market in the world is air transport of passengers and goods and buoyant aerial vehicles are one of the potential candidates for such applications. Aerodynamic and stability characteristics of such vehicles are critical issues of design and any new such design should exhibit longitudinal and directional stability. A generic model of hybrid buoyant aerial vehicle, consisting of fuselage similar to a hull of airship, was numerically tested by using Aircraft DATCOM to get first-hand knowledge about the general trends of aerodynamic and stability parameters. Most of such tools are limited to well-defined conventional aircraft configurations. But based on the presented results, it can be revealed that such tools can be used for hybrid buoyant aerial vehicles as well. Presented results will be validated in future by wind tunnel testing. 2015-05-15 Conference or Workshop Item PeerReviewed application/pdf en http://irep.iium.edu.my/46469/1/AeroHybrid_Buoyant.pdf application/pdf en http://irep.iium.edu.my/46469/4/62nd_CASI_Aeronautics_Conference_and_AGM_3rd_GARDN_Conference_Programme.pdf application/pdf en http://irep.iium.edu.my/46469/5/62nd_CASI_abstract.pdf UlHaque, Anwar and Asrar, Waqar and Omar, Ashraf A. and Sulaeman, Erwin and Syed Mohamed Ali, Jaffar (2015) Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed. In: 62nd Canadian Aerospace Institute Conference (Aero 2015), 19 - 21 May 2015, Montreal, Canada. (In Press) http://programme.exordo.com/aero2015/
repository_type	Digital Repository
institution_category	Local University
institution	International Islamic University Malaysia
building	IIUM Repository
collection	Online Access
language	English English English
topic	TL Motor vehicles. Aeronautics. Astronautics
spellingShingle	TL Motor vehicles. Aeronautics. Astronautics UlHaque, Anwar Asrar, Waqar Omar, Ashraf A. Sulaeman, Erwin Syed Mohamed Ali, Jaffar Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
description	It is well known that a big aviation market in the world is air transport of passengers and goods and buoyant aerial vehicles are one of the potential candidates for such applications. Aerodynamic and stability characteristics of such vehicles are critical issues of design and any new such design should exhibit longitudinal and directional stability. A generic model of hybrid buoyant aerial vehicle, consisting of fuselage similar to a hull of airship, was numerically tested by using Aircraft DATCOM to get first-hand knowledge about the general trends of aerodynamic and stability parameters. Most of such tools are limited to well-defined conventional aircraft configurations. But based on the presented results, it can be revealed that such tools can be used for hybrid buoyant aerial vehicles as well. Presented results will be validated in future by wind tunnel testing.
format	Conference or Workshop Item
author	UlHaque, Anwar Asrar, Waqar Omar, Ashraf A. Sulaeman, Erwin Syed Mohamed Ali, Jaffar
author_facet	UlHaque, Anwar Asrar, Waqar Omar, Ashraf A. Sulaeman, Erwin Syed Mohamed Ali, Jaffar
author_sort	UlHaque, Anwar
title	Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
title_short	Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
title_full	Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
title_fullStr	Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
title_full_unstemmed	Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed
title_sort	aerodynamics and static stability characteristics of a hybrid buoyant aerial vehicle at low speed
publishDate	2015
url	http://irep.iium.edu.my/46469/ http://irep.iium.edu.my/46469/ http://irep.iium.edu.my/46469/1/AeroHybrid_Buoyant.pdf http://irep.iium.edu.my/46469/4/62nd_CASI_Aeronautics_Conference_and_AGM_3rd_GARDN_Conference_Programme.pdf http://irep.iium.edu.my/46469/5/62nd_CASI_abstract.pdf
first_indexed	2023-09-18T21:06:10Z
last_indexed	2023-09-18T21:06:10Z
_version_	1777410948003266560

Aerodynamics and Static Stability Characteristics of a Hybrid Buoyant Aerial Vehicle at Low Speed

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