Development Of Design And Manufacturing Of A Fixed Wing Radio Controlled Micro Air Vehicle (Mav)

dc.contributor.author	Hossain, M A
dc.contributor.author	Hasan, F
dc.contributor.author	Seraz, A F M T
dc.contributor.author	Rajib, S A
dc.date.accessioned	2015-09-09T07:46:46Z
dc.date.available	2015-09-09T07:46:46Z
dc.date.issued	2011-02
dc.description.abstract	Micro Air Vehicles (MAVs) are a new type of aircraft maturing day by day and have reached unprecedented levels of growth recently. Similarly to larger Unmanned Air Vehicles (UAVs), MAVs have enormous potential in applications, both military and civilian, like reconnaissance over battlefields and surveillance of urban areas, data relay, air sampling etc. This article describes the development and selection of a fixed wing MAV with the analysis of simulated results. High wing theory with NACA 4412 aerofoil’s analytical data has been used to practically predict the performance of the MAV.
dc.identifier.other	https://dspace.mist.ac.bd/server/api/core/items/96d01d7c-64e3-4bda-ba9c-da85255282dd
dc.identifier.uri	http://hdl.handle.net/123456789/202
dc.language.iso	en
dc.publisher	R&D Wing, MIST
dc.source	MIST Digital Archive
dc.subject	Fixed wing, MAV, NACA 4412, Clark Y.
dc.title	Development Of Design And Manufacturing Of A Fixed Wing Radio Controlled Micro Air Vehicle (Mav)
dc.type	Article

Files

Now showing 1 - 1 of 1