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...

Deskribapen osoa

Gorde:
Xehetasun bibliografikoak
Egile Nagusiak: Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
Formatua: Tesis
Hizkuntza:ingelesa
Argitaratua: Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
Gaiak:
Sarrera elektronikoa:http://hdl.handle.net/123456789/245
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