An analysis of the efficiency of the functional matching between a flying wing MAV airframe and different types of micro propellers

This paper aims to present specific methods for optimizing the design of micro propellersfor small Reynolds numbers. In order to better understand the aim of this contribution, the effects of amicro propeller on the aerodynamic surfaces of a micro air vehicle (for example a flying wingconfiguration)...

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Bibliographic Details
Main Authors: Ionică CÎRCIU, Mircea BOSCOIANU
Format: Article
Language:English
Published: National Institute for Aerospace Research “Elie Carafoli” - INCAS 2011-03-01
Series:INCAS Bulletin
Subjects:
Online Access:http://bulletin.incas.ro/files/mircea_boscoianu_v3is1_full.pdf