2014
DOI: 10.4236/jamp.2014.212117
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Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion

Abstract: Development of flapping wing aerial vehicle (FWAV) has been of interest in the aerospace community with ongoing research into unsteady and low Reynolds number aerodynamics based on the vortex lattice method. Most of the previous research has been about pitching and plunging motion of the FWAV. With pitching and flapping motion of FMAV, people usually study it by experiment, and little work has been done by numerical calculation. In this paper, three-dimension unsteady vortex lattice method is applied to study … Show more

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Cited by 10 publications
(7 citation statements)
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“…Within the physical assumptions limitations; encouraging qualitative agreements or better have been indicated, which meet the proof of concept objectives of the present work. For the bi-wing flapping ornithopter, judging from the production of aerodynamic forces, the present flapping-wing model performance is comparable to those studied by Yu, et al [20]. The analysis and simulation by…”
Section: Simulation Resultssupporting
confidence: 79%
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“…Within the physical assumptions limitations; encouraging qualitative agreements or better have been indicated, which meet the proof of concept objectives of the present work. For the bi-wing flapping ornithopter, judging from the production of aerodynamic forces, the present flapping-wing model performance is comparable to those studied by Yu, et al [20]. The analysis and simulation by…”
Section: Simulation Resultssupporting
confidence: 79%
“…In Figure 8 and Table 2, geometric and kinematic parameters used by Yu, et al [20] are taken into account to produce comparable qualitative and quantitative agreements with their results; the latter were calculated using three-dimensional unsteady vortex lattice method Figure 9.…”
Section: Variation Of Oscillatory Articulation Of the Bi-wingmentioning
confidence: 68%
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“…i.e. ~ 300g and is given by the relation [6,7], (2) Considering the above equation, we get flapping frequency as 5.88Hz…”
Section: Figure 3 Motor Specificationsmentioning
confidence: 99%
“…Even while it does not considerably address the problems with energy storage and actuator downsizing that currently impede MAV development, a robot with a 0.8-meter wingspan is a significant step toward addressing the control concerns that these projects will soon face. We believe that despite the Phoenix being several orders of magnitude larger than the MAVs now under development, many of the issues with stabilizing and extracting agility from them have been preserved due to the scaling up [6].…”
Section: Introductionmentioning
confidence: 99%