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...

Celý popis

Podrobná bibliografie

Hlavní autoři:	Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
Médium:	Diplomová práce
Jazyk:	angličtina
Vydáno:	Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
Témata:	STRUCTURAL DESIGN, ANALYSIS, FLIGHT, UNMANNED AERIAL VEHICLE, AEROFOIL, SHAPED FUSELAGE
On-line přístup:	http://hdl.handle.net/123456789/245
Tagy:	Přidat tag Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!