AEROSTATIC AND AERODYNAMIC MODULES OF A HYBRID BUOYANT AIRCRAFT: AN ANALYTICAL APPROACH

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 aircrafts have two different modules to balance the weight of aircraft; aerostatic module and aerodynamic module. Both these modules are to be treated se...

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Main Authors: Anwar Ul Haque, WAQAR ASRAR, ASHRAF A. OMAR, ERWIN SULAEMAN, MOHAMED J.S. ALI
Format: Article
Language:English
Published: IIUM Press, International Islamic University Malaysia 2015-05-01
Series:International Islamic University Malaysia Engineering Journal
Online Access:http://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/532
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spelling doaj-096ec07b1f344596b5d2b89ff74cb2ed2020-11-25T03:49:14ZengIIUM Press, International Islamic University MalaysiaInternational Islamic University Malaysia Engineering Journal1511-788X2289-78602015-05-0116110.31436/iiumej.v16i1.532AEROSTATIC AND AERODYNAMIC MODULES OF A HYBRID BUOYANT AIRCRAFT: AN ANALYTICAL APPROACHAnwar Ul Haque0WAQAR ASRAR1ASHRAF A. OMAR2ERWIN SULAEMAN3MOHAMED J.S. ALI4Department of Mechanical Engineering, IIUMDepartment of Mechanical Engineering, International Islamic University MalaysiaDepartment of Mechanical Engineering, International Islamic University MalaysiaDepartment of Mechanical Engineering, International Islamic University MalaysiaDepartment of Mechanical Engineering, International Islamic University Malaysia An analytical approach is essential for the estimation of the requirements of aerodynamic and aerostatic lift for a hybrid buoyant aircraft. Such aircrafts 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 disussed and it is precieved that it will provide a strating point for better understanding of design anatomy of such aircraft. http://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/532
collection DOAJ
language English
format Article
sources DOAJ
author Anwar Ul Haque
WAQAR ASRAR
ASHRAF A. OMAR
ERWIN SULAEMAN
MOHAMED J.S. ALI
spellingShingle Anwar Ul Haque
WAQAR ASRAR
ASHRAF A. OMAR
ERWIN SULAEMAN
MOHAMED J.S. ALI
AEROSTATIC AND AERODYNAMIC MODULES OF A HYBRID BUOYANT AIRCRAFT: AN ANALYTICAL APPROACH
International Islamic University Malaysia Engineering Journal
author_facet Anwar Ul Haque
WAQAR ASRAR
ASHRAF A. OMAR
ERWIN SULAEMAN
MOHAMED J.S. ALI
author_sort Anwar Ul Haque
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, International Islamic University Malaysia
series International Islamic University Malaysia Engineering Journal
issn 1511-788X
2289-7860
publishDate 2015-05-01
description An analytical approach is essential for the estimation of the requirements of aerodynamic and aerostatic lift for a hybrid buoyant aircraft. Such aircrafts 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 disussed and it is precieved that it will provide a strating point for better understanding of design anatomy of such aircraft.
url http://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/532
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AT waqarasrar aerostaticandaerodynamicmodulesofahybridbuoyantaircraftananalyticalapproach
AT ashrafaomar aerostaticandaerodynamicmodulesofahybridbuoyantaircraftananalyticalapproach
AT erwinsulaeman aerostaticandaerodynamicmodulesofahybridbuoyantaircraftananalyticalapproach
AT mohamedjsali aerostaticandaerodynamicmodulesofahybridbuoyantaircraftananalyticalapproach
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