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...
| Main Authors: | , , , , |
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| Format: | Proceeding Paper |
| Language: | English English English |
| Published: |
2015
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| Online Access: | 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 |
| _version_ | 1848782975454412800 |
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| 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 |
| building | IIUM Repository |
| collection | Online Access |
| 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. |
| first_indexed | 2025-11-14T16:14:00Z |
| format | Proceeding Paper |
| id | iium-46469 |
| institution | International Islamic University Malaysia |
| institution_category | Local University |
| language | English English English |
| last_indexed | 2025-11-14T16:14:00Z |
| publishDate | 2015 |
| recordtype | eprints |
| repository_type | Digital Repository |
| 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 Proceeding Paper 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/ |
| 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 |
| title | 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_short | 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 |
| topic | TL Motor vehicles. Aeronautics. Astronautics |
| 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 |