Conceptual design of a winged hybrid airship

• Main Authors: UlHaque, Anwar, Asrar, Waqar, Omar, Ashraf Ali, Sulaeman, Erwin, Ali, JS Mohamed
• Format: Conference or Workshop Item
• Language: English; English; English
• Published: 2014
• Subjects: TL500 Aeronautics
• 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
• Institution: Universiti Islam Antarabangsa Malaysia

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...