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

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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
Format: Thesis
Sprog:engelsk
Udgivet: Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
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STRUCTURAL DESIGN, ANALYSIS, FLIGHT, UNMANNED AERIAL VEHICLE, AEROFOIL, SHAPED FUSELAGE
Online adgang:http://hdl.handle.net/123456789/245
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