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Thrust-constrained parametric design of high-altitude propellers: a CFD and genetic algorithm co-optimization for low-reynolds number efficiency gains

Crossref DOI link: https://doi.org/10.1007/s40430-026-06318-5

Published Online: 2026-03-26

Published Print: 2026-04

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

Authors

Guan, Chenyang

Wang, Kelong

Wang, Chuan

Li, Nanyi https://orcid.org/0009-0007-0981-5002
Guo, Bing
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (52005282)

Natural Science Foundation of Qinghai Province (2021-ZJ-954Q)
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Text and Data Mining valid from 2026-03-26

Version of Record valid from 2026-03-26
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Article History

Received: 18 May 2025

Accepted: 5 January 2026

First Online: 26 March 2026

Declarations

:

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

: Not applicable.

: Not applicable.

: The authors consent to publish this article.

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