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- W2043506012 abstract "Flight testing methods are proposed to flnd the drag polar for small UAVs powered by electric motors with flxed-pitch propellers. Wind tunnel testing was used to characterize the propeller-motor e‐ciency. The drag polar was constructed using data from ∞ight tests at various airspeeds. The proposed methods are implemented for a small UAV. A drag polar was found for this aircraft with CDo equal to 0.021, K1 equal to 0.229, and K2 equal to -0.056." @default.
- W2043506012 created "2016-06-24" @default.
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- W2043506012 date "2005-06-18" @default.
- W2043506012 modified "2023-10-16" @default.
- W2043506012 title "Flight Testing of Small, Electric Powered Unmanned Aerial Vehicles" @default.
- W2043506012 cites W4211197929 @default.
- W2043506012 doi "https://doi.org/10.2514/6.2005-7654" @default.
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