Conceptual design of a winged hybrid airship

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Conceptual design of a winged hybrid airship

The present study focuses on the sizing and aerodynamic contour design of a two-seater 1000 kg gross take-off mass winged hybrid airship. Unlike the conventional hybrid airships, which stay aloft and takeoff with the help of VTOL propulsion systems, a winged hybrid airship requires a certain s...

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Bibliographic Details
Main Authors:	UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Ali, JS Mohamed
Format:	Proceeding Paper
Language:	English English English
Published:	2014
Subjects:	TL500 Aeronautics
Online Access:	http://irep.iium.edu.my/38913/ http://irep.iium.edu.my/38913/1/LTA_01_1888278.pdf http://irep.iium.edu.my/38913/4/AIAA_Aviation_2014_conf_proceedings.docx http://irep.iium.edu.my/38913/5/14-315_Aviation_2014_Final_Program_FINALv2_LowRes.pdf

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