DEVELOPMENT OF DESIGN AND MANUFACTURING OF A FIXED WING RADIO CONTROLLED MICRO AIR VEHICLE (MAV)
DOI:
https://doi.org/10.47981/j.mijst.03(01)2011.19(%25p)Keywords:
Fixed wing, MAV, NACA 4412, Clark Y.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.
Downloads
References
Downloads
Published
Issue
Section
License
Copyright (c) 2019 MIST INTERNATIONAL JOURNAL OF SCIENCE AND TECHNOLOGY
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.
MIJST follows the open access policy.
This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License. This allows anyone to copy, share, distribute, and modify the work for non-commercial purposes, where the original work and source should be properly credited.
