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...

Volledige beschrijving

Bibliografische gegevens

Hoofdauteurs:	Rahman, Irfanur, Asaduzzaman, K. M., Arman, Arif
Formaat:	Thesis
Taal:	Engels
Gepubliceerd in:	Department of Mechanical Engineering (ME) Military Institute of Science and Technology (MIST) 2016
Onderwerpen:	STRUCTURAL DESIGN, ANALYSIS, FLIGHT, UNMANNED AERIAL VEHICLE, AEROFOIL, SHAPED FUSELAGE
Online toegang:	http://hdl.handle.net/123456789/245
Tags:	Voeg label toe Geen labels, Wees de eerste die dit record labelt!