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• W2460673108 endingPage "046001" @default.
• W2460673108 startingPage "046001" @default.
• W2460673108 abstract "This experimental study investigates the effect of three parameters: wing aspect ratio (AR), wing offset, and flapping frequency, on thrust generation and power consumption of a flapping-wing system based on a rack-pinion mechanism. The new flapping-wing system is simple but robust, and is able to create a large flapping amplitude. The thrust measured by a load cell reveals that for a given power, the flapping-wing system using a higher wing AR produces larger thrust and higher flapping frequency at the wing offset of 0.15 or 0.20 ( is the mean chord) than other wing offsets. Of the three parameters, the flapping frequency plays a more significant role on thrust generation than either the wing AR or the wing offset. Based on the measured thrusts, an empirical equation for thrust prediction is suggested, as a function of wing area, flapping frequency, flapping angle, and wing AR. The difference between the predicted and measured thrusts was less than 7%, which proved that the empirical equation for thrust prediction is reasonable. On average, the measured power consumption to flap the wings shows that 46.5% of the input power is spent to produce aerodynamic forces, 14.0% to overcome inertia force, 9.5% to drive the rack-pinion-based flapping mechanism, and 30.0% is wasted as the power loss of the installed motor. From the power analysis, it is found that the wing with an AR of 2.25 using a wing offset of 0.20 showed the optimal power loading in the flapping-wing system. In addition, the flapping frequency of 25 Hz is recommended as the optimal frequency of the current flapping-wing system for high efficiency, which was 48.3%, using a wing with an AR of 2.25 and a wing offset of 0.20 in the proposed design." @default.
• W2460673108 created "2016-07-22" @default.
• W2460673108 creator A5014683378 @default.
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• W2460673108 date "2016-06-20" @default.
• W2460673108 modified "2023-09-26" @default.
• W2460673108 title "Experimental study on thrust and power of flapping-wing system based on rack-pinion mechanism" @default.
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• W2460673108 doi "https://doi.org/10.1088/1748-3190/11/4/046001" @default.
• W2460673108 hasPubMedId "https://pubmed.ncbi.nlm.nih.gov/27321705" @default.
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