Author:
Mieloszyk Jacek,Galinski Cezary
Abstract
Two configurations of micro-airplanes are compared in this paper. The first, very innovative one, has a propeller working in a slot in the middle of the wing. The second airplane has more classical configuration with a pusher propeller. Advantages and disadvantages of both configurations are evaluated, which makes it possible to assess what are the best possible mission types for each micro-airplane.
Subject
Mechanical Engineering,Mechanics of Materials
Cited by
3 articles.
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1. An Efficient Design of the Piezoresistive Pressure Sensor Applied for Micro Aerial Vehicle;The International Journal of Integrated Engineering;2023-04-05
2. Propeller locations study of a generic delta wing UAV model;Aircraft Engineering and Aerospace Technology;2020-11-30
3. Numerical investigation of mutual interaction between a pusher propeller and a fuselage;Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering;2020-06-08