Haithem Taha
Title
Cited by
Cited by
Year
State-space representation of the unsteady aerodynamics of flapping flight
HE Taha, MR Hajj, PS Beran
Aerospace Science and Technology 34, 1-11, 2014
1412014
Flight dynamics and control of flapping-wing MAVs: a review
HE Taha, MR Hajj, AH Nayfeh
Nonlinear Dynamics 70 (2), 907-939, 2012
1362012
The need for higher-order averaging in the stability analysis of hovering, flapping-wing flight
HE Taha, S Tahmasian, CA Woolsey, AH Nayfeh, MR Hajj
Bioinspiration & biomimetics 10 (1), 016002, 2015
592015
Longitudinal flight dynamics of hovering MAVs/insects
HE Taha, MR Hajj, AH Nayfeh
Journal of Guidance, Control, and Dynamics 37 (3), 970-979, 2014
462014
Wing kinematics optimization for hovering micro air vehicles using calculus of variation
HE Taha, MR Hajj, AH Nayfeh
Journal of Aircraft 50 (2), 610-614, 2013
442013
Geometrically-exact unsteady model for airfoils undergoing large amplitude maneuvers
Z Yan, HE Taha, MR Hajj
Aerospace Science and Technology 39, 293-306, 2014
342014
Viscous extension of potential-flow unsteady aerodynamics: the lift frequency response problem
H Taha, AS Rezaei
Journal of Fluid Mechanics 868, 141-175, 2019
312019
Geometric control approach to longitudinal stability of flapping flight
HE Taha, CA Woolsey, MR Hajj
Journal of Guidance, Control, and Dynamics 39 (2), 214-226, 2016
292016
Effect of the aerodynamic-induced parametric excitation on the longitudinal stability of hovering MAVs/insects
HE Taha, AH Nayfeh, MR Hajj
Nonlinear Dynamics 78 (4), 2399-2408, 2014
292014
Unsteady nonlinear aerodynamics of hovering mavs/insects
H Taha, M Hajj
51st AIAA Aerospace Sciences Meeting Including the New Horizons Forum and …, 2013
282013
Measurement and modeling of lift enhancement on plunging airfoils: A frequency response approach
MY Zakaria, HE Taha, MR Hajj
Journal of Fluids and Structures 69, 187-208, 2017
272017
Nonlinear characteristics of an autoparametric vibration system
Z Yan, HE Taha, T Tan
Journal of sound and vibration 390, 1-22, 2017
252017
Effects of aerodynamic modeling on the optimal wing kinematics for hovering MAVs
Z Yan, HE Taha, MR Hajj
Aerospace Science and Technology 45, 39-49, 2015
232015
Design optimization of flapping ornithopters: the pterosaur replica in forward flight
MY Zakaria, HE Taha, MR Hajj
Journal of Aircraft 53 (1), 48-59, 2016
222016
Unsteady viscous lift frequency response using the triple deck theory
HE Taha, AS Rezaei
2018 AIAA Aerospace Sciences Meeting, 0038, 2018
182018
Optimal transition of flapping wing micro-air vehicles from hovering to forward flight
AA Hussein, AE Seleit, HE Taha, MR Hajj
Aerospace Science and Technology 90, 246-263, 2019
172019
Geometric control formulation and nonlinear controllability of airplane flight dynamics
AM Hassan, HE Taha
Nonlinear Dynamics 88 (4), 2651-2669, 2017
172017
Computational study of lift frequency responses of pitching airfoils at low Reynolds numbers
AS Rezaei, HE Taha
55th AIAA Aerospace Sciences Meeting, 0716, 2017
172017
Optimal morphing–augmented dynamic soaring maneuvers for unmanned air vehicle capable of span and sweep morphologies
I Mir, A Maqsood, SA Eisa, H Taha, S Akhtar
Aerospace Science and Technology 79, 17-36, 2018
162018
A controllability perspective of dynamic soaring
I Mir, H Taha, SA Eisa, A Maqsood
Nonlinear Dynamics 94 (4), 2347-2362, 2018
142018
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