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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| Main Authors: | , |
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| Format: | Article |
| Language: | English |
| Published: |
Aerospace Society Malaysia
2023
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| Online Access: | http://psasir.upm.edu.my/id/eprint/107583/1/107583.pdf http://psasir.upm.edu.my/id/eprint/107583/ https://www.aerosmalaysia.my/aeros_journal/index.php/journal/article/view/4 |
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