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
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.
This journal provides immediate open access to its content on the principle that making research freely available to the public supports a greater global exchange of knowledge. Users are permitted to read, download, copy, distribute, print, search, or link to the full texts of the articles, provided that appropriate credit is given to the original authors.
