Haithem E. Taha, Ph.D.
Affiliations: | 2013 | Virginia Polytechnic Institute and State University, Blacksburg, VA, United States |
Area:
Aerospace Engineering, Mechanical EngineeringGoogle:
"Haithem Taha"Parents
Sign in to add mentor| Ali H. Nayfeh | grad student | 2013 | Virginia Tech | |
| (Mechanics of Flapping Flight: Analytical Formulations of Unsteady Aerodynamics, Kinematic Optimization, Flight Dynamics, and Control.) | ||||
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Publications
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| Deb D, Huang K, Verma A, et al. (2023) Thrust enhancement and degradation mechanisms due to self-induced vibrations in bio-inspired flying robots. Scientific Reports. 13: 18317 |
| Mir I, Eisa SA, Taha HE, et al. (2021) A stability perspective of bio-inspired UAVs performing dynamic soaring optimally. Bioinspiration & Biomimetics |
| Taha HE, Kiani M, Hedrick TL, et al. (2020) Vibrational control: A hidden stabilization mechanism in insect flight. Science Robotics. 5 |
| Taha HE, Rezaei AS. (2020) On the high-frequency response of unsteady lift and circulation: A dynamical systems perspective Journal of Fluids and Structures. 93: 102868 |
| Santos CRd, Pacheco DRQ, Taha HE, et al. (2020) Nonlinear modeling of electro-aeroelastic dynamics of composite beams with piezoelectric coupling Composite Structures. 112968 |
| Maggia M, Eisa SA, Taha HE. (2020) On higher-order averaging of time-periodic systems: reconciliation of two averaging techniques Nonlinear Dynamics. 99: 813-836 |
| Taha H, Rezaei AS. (2019) Viscous extension of potential-flow unsteady aerodynamics: the lift frequency response problem Journal of Fluid Mechanics. 868: 141-175 |
| Hussein AA, Seleit AE, Taha HE, et al. (2019) Optimal transition of flapping wing micro-air vehicles from hovering to forward flight Aerospace Science and Technology. 90: 246-263 |
| Hassan AM, Taha HE. (2019) Differential-Geometric-Control Formulation of Flapping Flight Multi-body Dynamics Journal of Nonlinear Science. 29: 1379-1417 |
| Hussein AA, Taha HE, Ragab S, et al. (2018) A variational approach for the dynamics of unsteady point vortices Aerospace Science and Technology. 78: 559-568 |