תמונות העטיפה

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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שמור ב:
Main Authors: Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
פורמט: Thesis
שפה:אנגלית
יצא לאור: Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
נושאים:
STRUCTURAL DESIGN, ANALYSIS, FLIGHT, UNMANNED AERIAL VEHICLE, AEROFOIL, SHAPED FUSELAGE
גישה מקוונת:http://hdl.handle.net/123456789/245
תגים: הוספת תג
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אינטרנט

http://hdl.handle.net/123456789/245

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