Aiaa Aviation 2021 Forum 2021
DOI: 10.2514/6.2021-2598.c1
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Correction: Robust modeling and optimal design of rotors using blade element momentum theory

Abstract: In section IV.B on page 13, the last sentence of the first paragraph should read that in Fig. 4, the output of the idealloading design method is shown in red, not blue, and the result of the blade element momentum (BEM) optimization is shown in blue, not red.

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