2019
DOI: 10.2514/1.c035239
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Computational and Experimental Investigation of a Flapping-Wing Micro Air Vehicle in Hover

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Cited by 10 publications
(7 citation statements)
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“…Based on the above studies, the dynamic model of the robot under the disturbances was established for studying the dynamic performances of the robot. Specially, I have tried to establish the dynamic model of the robot under randomly uncertain disturbances by using the Reynolds-averaged Navier-Stokes (RANS) equation [41][42][43]. However, it is difficult to obtain simulation results as the calculation amount is very large.…”
Section: Plos Onementioning
confidence: 99%
“…Based on the above studies, the dynamic model of the robot under the disturbances was established for studying the dynamic performances of the robot. Specially, I have tried to establish the dynamic model of the robot under randomly uncertain disturbances by using the Reynolds-averaged Navier-Stokes (RANS) equation [41][42][43]. However, it is difficult to obtain simulation results as the calculation amount is very large.…”
Section: Plos Onementioning
confidence: 99%
“…Computational fluid dynamics modelling. We performed three-dimensional Reynolds-averaged Navier-Stokes (RANS) simulations of the aerodynamics of the right wing of Calliphora using the OVERTURNS solver [60,61]. We simulated a reference condition of level symmetric forward flight with a freestream velocity of 𝑈 ∞ = 0.8509 m s -1 and a wingbeat frequency of 𝑓 = 166.188 Hz, corresponding to the mean values measured for these variables over the 2,708 wingbeats whose kinematics we had recorded (see above).…”
Section: Aerodynamic Modelling Of Stability and Control Derivativesmentioning
confidence: 99%
“…Therefore, it is evident that due to vortices at the tip and root that interfere with the wing during the flapping period, unsteady lift and drag are produced. For assessing the performance of geometry and kinematic parameters of flapping-wing vehicles, power loading is more appropriate than the lift-to-drag ratio [ 73 ].…”
Section: Lift Generation Mechanismsmentioning
confidence: 99%