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Effects of wall cooling on hypersonic shock wave turbulent boundary layer interaction – CORRIGENDUM

Published online by Cambridge University Press:  09 December 2025

Z. Tang Open the ORCID record for Z. Tang [Opens in a new window] ,
H. Xu ,
X. Li  and
J. Ren
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Abstract

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Type
Corrigendum
Information
The Aeronautical Journal , First View , pp. 1
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Copyright
© The Author(s), 2025. Published by Cambridge University Press on behalf of Royal Aeronautical Society

The authors regret that authors’ names were incorrectly cited in the original article as A.Z. Tang, B.H. Xu, C.X. Li and D.J. Ren.

The authors’ names are as follows:

Z. Tang, H. Xu, X. Li and J. Ren

References

Tang, Z., Xu, H., Li, X., and Ren, J., Effects of wall cooling on hypersonic shock wave turbulent boundary layer interaction, The Aeronautical Journal, 2025, 129, (1341), pp 3184–3201, https://doi.org/10.1017/aer.2025.10049.CrossRefGoogle Scholar