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Combination of Advanced Actuator Line/Disk Model and a High-Order Unstructured Finite Volume Solver for Helicopter Rotors

This version is not peer-reviewed.

Submitted:

13 November 2023

Posted:

14 November 2023

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Abstract
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Engineering  -   Aerospace Engineering
Copyright: This open access article is published under a Creative Commons CC BY 4.0 license, which permit the free download, distribution, and reuse, provided that the author and preprint are cited in any reuse.
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