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- W2315661006 abstract "This paper describes a series of systematic experimental studies conducted to optimize the performance of a MAV scale cycloidal rotor. Parametric studies were performed to study the effects of blade airfoil section, blade pitching amplitude, asymmetric pitching, location of blade pitching axis and number of blades (at constant solidity) on the performance of the cycloidal rotor. Higher blade pitch angles were found to improve thrust and increase the power loading (thrust per unit power) of the cycloidal rotor. Asymmetric pitching, with a higher pitch angle at the top than at the bottom of the circular blade trajectory, produced better power loading. The optimum pitching axis location was observed to be around 25-35% of the blade chord. For a constant solidity, the rotor with lesser number of blades produced higher thrust and a 2-bladed rotor had the best power loading. Using the results from these parametric studies, an optimized cycloidal rotor with a significantly improved power loading over a conventional MAV rotor was developed." @default.
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- W2315661006 date "2011-01-04" @default.
- W2315661006 modified "2023-09-27" @default.
- W2315661006 title "Experimental Optimization and Performance Analysis of a MAV Scale Cycloidal Rotor" @default.
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- W2315661006 doi "https://doi.org/10.2514/6.2011-821" @default.
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