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Compliant mechanism design of combined aircraft wing for stable separation – CORRIGENDUM

Published online by Cambridge University Press:  16 September 2024

Q. Zhang ,
S. Jia ,
J. Chen  and
J. Zhang
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Abstract

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Keywords

Aircraft designSeparation mechanism designSeparation kineticsAerodynamics

Information

Type
Corrigendum
Information
The Aeronautical Journal , First View , pp. 1
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Copyright
© The Author(s), 2024. Published by Cambridge University Press on behalf of Royal Aeronautical Society

The originally published article contained an error in the Acknowledgements, which has now been updated from: ‘Technology Special Project with the agreement number 2021-JCIO-JJ-0233’ to ‘Technology Special Project with the agreement number 2021-JCJQ-JJ-0233’.

References

Zhang, Q., Jia, S., Chen, J. and Zhang, J. Compliant mechanism design of combined aircraft wing for stable separation. The Aeronautical Journal, https://doi.org/10.1017/aer.2024.12Google Scholar