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.	en_US
dc.description.sponsorship	R&D Wing	en_US
dc.identifier.uri	http://hdl.handle.net/123456789/202
dc.language.iso	en	en_US
dc.publisher	R&D Wing, MIST	en_US
dc.relation.ispartofseries	Galaxy (Dhaka) : The Annual Technical Journal of MIST;Volume 3, Number 3, February 2011
dc.subject	Fixed wing, MAV, NACA 4412, Clark Y.	en_US
dc.title	Development Of Design And Manufacturing Of A Fixed Wing Radio Controlled Micro Air Vehicle (Mav)	en_US
dc.type	Article	en_US

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