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Design method for hypersonic bump inlet based on transverse pressure gradient

Crossref DOI link: https://doi.org/10.1631/jzus.A2100532

Published Online: 2022-07-07

Published Print: 2022-06

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

Authors

Xu, Shang-cheng https://orcid.org/0000-0002-0717-8392
Wang, Yi https://orcid.org/0000-0002-3657-9769
Wang, Zhen-guo

Fan, Xiao-qiang

Xiong, Bing
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Text and Data Mining valid from 2022-06-01

Version of Record valid from 2022-06-01
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Article History

Received: 21 October 2021

Accepted: 4 January 2022

First Online: 7 July 2022