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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書誌詳細

主要な著者:	Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
フォーマット:	学位論文
言語:	英語
出版事項:	Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
主題:	STRUCTURAL DESIGN, ANALYSIS, FLIGHT, UNMANNED AERIAL VEHICLE, AEROFOIL, SHAPED FUSELAGE
オンライン･アクセス:	http://hdl.handle.net/123456789/245
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