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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| Main Authors: | , , , , |
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| Format: | Conference or Workshop Item |
| Language: | English English English |
| Published: |
2014
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| Subjects: | |
| Online Access: | 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 http://irep.iium.edu.my/38913/ http://www.aiaa.org/Secondary.aspx?id=18593 |
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| Institution: | Universiti Islam Antarabangsa Malaysia |
| Language: | English English English |