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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Main Authors:	Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
格式:	Thesis
語言:	英语
出版:	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
在線閱讀:	http://hdl.handle.net/123456789/245
標簽:	添加標簽 沒有標簽, 成為第一個標記此記錄!