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Numerical investigation of an active Gurney flap performance in a new flow control strategy to reduce dynamic stall effects of helicopter blade section in forward flight condition

Crossref DOI link: https://doi.org/10.1007/s40430-025-05561-6

Published Online: 2025-04-21

Published Print: 2025-05

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Kargarian, Abbas

Karimian, S. M. Hossein https://orcid.org/0000-0002-1934-7413
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Text and Data Mining valid from 2025-04-21

Version of Record valid from 2025-04-21
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Article History

Received: 19 April 2024

Accepted: 25 March 2025

First Online: 21 April 2025

Declarations

:

: The authors declare that they have no known competing financial interests or personal relationships that could have appeared to influence the work reported in this paper.

: This declaration is “not applicable.”

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