Mowhoub, M., & Abdullah, E. J. (2023). Effects of flapping wing micro air vehicle's pitching angle on stability at low reynolds number. Aerospace Society Malaysia.
Chicago Style (17th ed.) CitationMowhoub, Mohamed, and Ermira Junita Abdullah. Effects of Flapping Wing Micro Air Vehicle's Pitching Angle on Stability at Low Reynolds Number. Aerospace Society Malaysia, 2023.
MLA (9th ed.) CitationMowhoub, Mohamed, and Ermira Junita Abdullah. Effects of Flapping Wing Micro Air Vehicle's Pitching Angle on Stability at Low Reynolds Number. Aerospace Society Malaysia, 2023.
Warning: These citations may not always be 100% accurate.