Please use this identifier to cite or link to this item: https://ptsldigital.ukm.my/jspui/handle/123456789/577619
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dc.contributor.authorHaque Anwar U (IIUM)
dc.contributor.authorAsrar Waqar (IIUM)
dc.contributor.authorOmar Ashraf A. (IIUM)
dc.contributor.authorSulaeman Erwin (IIUM)
dc.contributor.authorAli Mohamed J. S. (IIUM)
dc.date.accessioned2023-11-06T02:45:50Z-
dc.date.available2023-11-06T02:45:50Z-
dc.date.issued2015
dc.identifier.issn1511-788X
dc.identifier.otherukmvital:78389
dc.identifier.urihttps://ptsldigital.ukm.my/jspui/handle/123456789/577619-
dc.descriptionAn 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.
dc.language.isoen
dc.publisherInternational Islamic University Malaysia (IIUM)
dc.relation.haspartIIUM Engineering Journal
dc.relation.urihttp://journals.iium.edu.my/ejournal/index.php/iiumej/article/view/532/413
dc.subjectAerostatic lift
dc.subjectAerodynamic lift
dc.subjectHybrid bouyant aircraft
dc.subjectDrag polar
dc.titleAerostatic and aerodynamic modules of a hybrid buoyant aircraft : an analytical approach
dc.typeJournal Article
dc.format.volume16
dc.format.pages9-17
dc.identifier.callnoSiri TA1.I485
dc.format.issue1
Appears in Collections:Journal Content Pages/ Kandungan Halaman Jurnal

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