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A theoretical study of serrated leading edges in aerofoil and vortical gust interaction noise

Crossref DOI link: https://doi.org/10.1186/s42774-019-0010-y

Published Online: 2019-02-28

Published Print: 2019-12

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

Authors

Huang, Xun
Funding

Funding for this research was provided by:

National Natural Science Foundation of China (11772005, 91852201)

Ministry of Industry and Information Technology of the People's Republic of China (MJ-2015-F-012-03)

Research Grants Council of Hong Kong (16205317)
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Article History

Received: 23 January 2019

Accepted: 30 January 2019

First Online: 28 February 2019

Competing interests

: Not applicable.

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