2022
DOI: 10.1007/s42405-022-00445-8
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Experimental Study on the Wing Parameter Optimization of Flapping-Wing Aircraft Based on the Clap-and-Fling Mechanism

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Cited by 12 publications
(9 citation statements)
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“…The geometry and manufacturing process of the wings of the flapping-wing mechanism are described in Ref. [ 44 ]. The rigid leading edge and root rods ensure the stability of the flexible wing, enabling the shape and camber of the wing to change passively, similar to the wings of insects during flapping [ 45 , 46 ].…”
Section: Resultsmentioning
confidence: 99%
“…The geometry and manufacturing process of the wings of the flapping-wing mechanism are described in Ref. [ 44 ]. The rigid leading edge and root rods ensure the stability of the flexible wing, enabling the shape and camber of the wing to change passively, similar to the wings of insects during flapping [ 45 , 46 ].…”
Section: Resultsmentioning
confidence: 99%
“…Substituting Equation (20) into Equation (19), the constraint relationship between motor torque and gear ratio can be obtained according to the constraints.…”
Section: Selection Gear Ratiomentioning
confidence: 99%
“…T m = (I − 0.9) × 0.00318 (24) By substituting Equations ( 14), (20), and (24) into Equation ( 23), the efficiency of the motor can be obtained.…”
Section: Wind Tunnel Experiments the Flight Test Prototypementioning
confidence: 99%
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“…A flapping-wing mechanism exerts periodic oscillatory lift force which is produced by wings. The actuation could be generated by direct current (DC) or brushless motors plus a crank-and-gear mechanism [14,18,19]; it could be produced by servo motors [22], clap-and-fling mechanism [23], or by elastic actuation based on an inverted-cam mechanical mechanism [24]. Regardless of actuation type, the periodic transferred base-excitation force should be controlled [25].…”
Section: Introductionmentioning
confidence: 99%