Development of Design and Manufacturing of a Fixed Wing Radio Controlled Micro Air Vehicle (MAV)

Authors

  • MA Hossain Asst. Professor, Department of Mechanical Engineering, Military Institute of Science and Technology
  • F Hasan Student, Department of Mechanical Engineering, Military Institute of Science and Technology.
  • AFMT Seraz Student, Department of Mechanical Engineering, Military Institute of Science and Technology.
  • SA Rajib Student, Department of Mechanical Engineering, Military Institute of Science and Technology.

DOI:

https://doi.org/10.3329/mist.v3i0.8048

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.

KEY WORDS: Fixed wing; MAV; NACA 4412; Clark Y.

DOI: http://dx.doi.org/10.3329/mist.v3i0.8048

Downloads

Download data is not yet available.
Abstract
1491
PDF
2624

Downloads

How to Cite

Hossain, M., Hasan, F., Seraz, A., & Rajib, S. (2011). Development of Design and Manufacturing of a Fixed Wing Radio Controlled Micro Air Vehicle (MAV). MIST Journal: GALAXY (DHAKA), 3. https://doi.org/10.3329/mist.v3i0.8048

Issue

Vol. 3 (2011)

Section

Articles

License

All rights reserved. No part of this publication may be reproduced, stored in retrieval system, or transmitted in any form, or by any means, electrical, photocopying, recording, or otherwise, without the prior permission of the publisher.