Effects of flapping wing micro air vehicle's pitching angle on stability at low reynolds number

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Effects of flapping wing micro air vehicle's pitching angle on stability at low reynolds number

The instability of flapping wing aircrafts makes them difficult to control. As it is challenging to control and puts passengers at risk, it is not currently employed in modern aircraft technology. This study aims to analyze the aerodynamic coefficients of flapping wing aircraft at different flapping...

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Bibliographic Details
Main Authors:	Mowhoub, Mohamed, Abdullah, Ermira Junita
Format:	Article
Language:	English
Published:	Aerospace Society Malaysia 2023
Online Access:	http://psasir.upm.edu.my/id/eprint/107583/ http://psasir.upm.edu.my/id/eprint/107583/1/107583.pdf

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