Framework of conceptual design methodology for hybrid buoyant aircraft

Framework of conceptual design methodology for hybrid buoyant aircraft

For economic and `green' transportation, the concept of hybrid buoyant aircraft has recently become a research focus in the aerospace community. In the present work, a methodology is proposed to aid in the conceptual design of such aircraft, powered by internal combustion engines with either...

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Main Authors: UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Mohamed Ali, Jaffar Syed
Format: Article
Language:English
Published: Associazione Italiana di Aeronautica e Astronautica, Sede di Pisa 2016
Subjects:
TL500 Aeronautics
Online Access:http://irep.iium.edu.my/52613/
http://irep.iium.edu.my/52613/
http://irep.iium.edu.my/52613/
http://irep.iium.edu.my/52613/1/Framework%20for%20design%20of%20HBA%20-%20Aerotecnica%20missili.pdf
id iium-52613
recordtype eprints
spelling iium-526132016-11-11T02:52:51Z http://irep.iium.edu.my/52613/ Framework of conceptual design methodology for hybrid buoyant aircraft UlHaque, Anwar Asrar, Waqar Omar, Ashraf Ali Sulaeman, Erwin Mohamed Ali, Jaffar Syed TL500 Aeronautics For economic and `green' transportation, the concept of hybrid buoyant aircraft has recently become a research focus in the aerospace community. In the present work, a methodology is proposed to aid in the conceptual design of such aircraft, powered by internal combustion engines with either liquid hydrogen or gasoline as a fuel. Special emphasis is given to the sequence of procedures to be adopted at the conceptual design level highlighting a step by step methodology for the achievement of system design targets with the help of a design example. The proposed design synthesis methodology has given a base line for further design work on such aircraft at a conceptual level. Moreover, it will assist to provide qualitative as well as quantitative data for other design concepts of such hybrid configurations being considered in the conceptual design phase. Associazione Italiana di Aeronautica e Astronautica, Sede di Pisa 2016-04 Article PeerReviewed application/pdf en http://irep.iium.edu.my/52613/1/Framework%20for%20design%20of%20HBA%20-%20Aerotecnica%20missili.pdf UlHaque, Anwar and Asrar, Waqar and Omar, Ashraf Ali and Sulaeman, Erwin and Mohamed Ali, Jaffar Syed (2016) Framework of conceptual design methodology for hybrid buoyant aircraft. Aerotecnica Missili & Spazio = The Journal of Aerospace Science, Technology and Systems, 95 (2 (April-June)). pp. 99-110. http://131.114.27.37/index.php/AMS/article/view/273 10.19249/ams.v95i2.273
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
UlHaque, Anwar
Asrar, Waqar
Omar, Ashraf Ali
Sulaeman, Erwin
Mohamed Ali, Jaffar Syed
Framework of conceptual design methodology for hybrid buoyant aircraft
description For economic and `green' transportation, the concept of hybrid buoyant aircraft has recently become a research focus in the aerospace community. In the present work, a methodology is proposed to aid in the conceptual design of such aircraft, powered by internal combustion engines with either liquid hydrogen or gasoline as a fuel. Special emphasis is given to the sequence of procedures to be adopted at the conceptual design level highlighting a step by step methodology for the achievement of system design targets with the help of a design example. The proposed design synthesis methodology has given a base line for further design work on such aircraft at a conceptual level. Moreover, it will assist to provide qualitative as well as quantitative data for other design concepts of such hybrid configurations being considered in the conceptual design phase.
format Article
author UlHaque, Anwar
Asrar, Waqar
Omar, Ashraf Ali
Sulaeman, Erwin
Mohamed Ali, Jaffar Syed
author_facet UlHaque, Anwar
Asrar, Waqar
Omar, Ashraf Ali
Sulaeman, Erwin
Mohamed Ali, Jaffar Syed
author_sort UlHaque, Anwar
title Framework of conceptual design methodology for hybrid buoyant aircraft
title_short Framework of conceptual design methodology for hybrid buoyant aircraft
title_full Framework of conceptual design methodology for hybrid buoyant aircraft
title_fullStr Framework of conceptual design methodology for hybrid buoyant aircraft
title_full_unstemmed Framework of conceptual design methodology for hybrid buoyant aircraft
title_sort framework of conceptual design methodology for hybrid buoyant aircraft
publisher Associazione Italiana di Aeronautica e Astronautica, Sede di Pisa
publishDate 2016
url http://irep.iium.edu.my/52613/
http://irep.iium.edu.my/52613/
http://irep.iium.edu.my/52613/
http://irep.iium.edu.my/52613/1/Framework%20for%20design%20of%20HBA%20-%20Aerotecnica%20missili.pdf
first_indexed 2023-09-18T21:14:30Z
last_indexed 2023-09-18T21:14:30Z
_version_ 1777411472257712128

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