STRUCTURAL DESIGN, ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE

This project and dissertation is a significant outcome of supreme guidance and concentrated team effort. We respectfully acknowledge the cordial help of individuals who played distinct role for the successful accomplishment of the project. We offer our deepest gratitude to our supervisor Wg Cdr Dr G...

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Asıl Yazarlar: Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
Materyal Türü: Tez
Dil:İngilizce
Baskı/Yayın Bilgisi: Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
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Online Erişim:http://hdl.handle.net/123456789/245
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STRUCTURAL DESIGN ANALYSIS AND FLIGHT TEST OF AN UNMANNED AERIAL VEHICLE (UAV) HAVING AEROFOIL SHAPED FUSELAGE /

Baskı/Yayın Bilgisi c2014.
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