Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach
An analytical approach is essential for the estimation of the requirements of aerodynamic and aerostatic lift for a hybrid buoyant aircraft. Such aircraft have two different modules to balance the weight of aircraft; aerostatic module and aerodynamic module. Both these modules are to be treated sep...
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iium-442352017-11-02T07:05:33Z http://irep.iium.edu.my/44235/ Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach UlHaque, Anwar Asrar, Waqar Omar, Ashraf Ali Sulaeman, Erwin Syed Mohamed Ali, Jaffar TL500 Aeronautics An analytical approach is essential for the estimation of the requirements of aerodynamic and aerostatic lift for a hybrid buoyant aircraft. Such aircraft have two different modules to balance the weight of aircraft; aerostatic module and aerodynamic module. Both these modules are to be treated separately for estimation of the mass budget of propulsion systems and required power. In the present work, existing relationships of aircraft and airship are reviewed for its further application for these modules. Limitations of such relationships are also discussed and they provide a starting point for better understanding of design methodology of such aircraft. IIUM Press 2015-06 Article PeerReviewed application/pdf en http://irep.iium.edu.my/44235/1/Aerostatic_and_aerodyn_analysis-IIUM_EJ.pdf application/pdf en http://irep.iium.edu.my/44235/4/44235_Aerostatic_and_aerodynamic_modules_of_a_hybrid_buoyant_aircraft_WOS.pdf UlHaque, Anwar and Asrar, Waqar and Omar, Ashraf Ali and Sulaeman, Erwin and Syed Mohamed Ali, Jaffar (2015) Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach. IIUM Engineering Journal, 16 (1). pp. 9-17. ISSN 2289-7860 (O), 1511-788X (P) E-ISSN 2289-7860 http://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/532 |
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International Islamic University Malaysia |
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language |
English English |
topic |
TL500 Aeronautics |
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TL500 Aeronautics UlHaque, Anwar Asrar, Waqar Omar, Ashraf Ali Sulaeman, Erwin Syed Mohamed Ali, Jaffar Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
description |
An analytical approach is essential for the estimation of the requirements of aerodynamic and aerostatic lift for a hybrid buoyant aircraft. Such aircraft have two
different modules to balance the weight of aircraft; aerostatic module and aerodynamic module. Both these modules are to be treated separately for estimation of the mass
budget of propulsion systems and required power. In the present work, existing relationships of aircraft and airship are reviewed for its further application for these
modules. Limitations of such relationships are also discussed and they provide a starting point for better understanding of design methodology of such aircraft. |
format |
Article |
author |
UlHaque, Anwar Asrar, Waqar Omar, Ashraf Ali Sulaeman, Erwin Syed Mohamed Ali, Jaffar |
author_facet |
UlHaque, Anwar Asrar, Waqar Omar, Ashraf Ali Sulaeman, Erwin Syed Mohamed Ali, Jaffar |
author_sort |
UlHaque, Anwar |
title |
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
title_short |
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
title_full |
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
title_fullStr |
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
title_full_unstemmed |
Aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
title_sort |
aerostatic and aerodynamic modules of a hybrid buoyant aircraft: an analytical approach |
publisher |
IIUM Press |
publishDate |
2015 |
url |
http://irep.iium.edu.my/44235/ http://irep.iium.edu.my/44235/ http://irep.iium.edu.my/44235/1/Aerostatic_and_aerodyn_analysis-IIUM_EJ.pdf http://irep.iium.edu.my/44235/4/44235_Aerostatic_and_aerodynamic_modules_of_a_hybrid_buoyant_aircraft_WOS.pdf |
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2023-09-18T21:02:54Z |
last_indexed |
2023-09-18T21:02:54Z |
_version_ |
1777410742335569920 |