Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft

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Effect of wing loading on gross takeoff mass of a hybrid buoyant aircraft

Aerostatic lift in a hybrid buoyant aircraft reduces the wing loading as well as the induced drag. This reduction is valid till pressure height. In this paper, the existing analytical relationships for the gross and net mass, as well as wing loading of standard aircraft, are modified to obtain new a...

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Bibliographic Details
Main Authors:	UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Ali, JS Mohamed
Format:	Article
Language:	English
Published:	Marques Engineering Ltd 2016
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/49541/ http://irep.iium.edu.my/49541/1/IJUSENG_HBA.pdf

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