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Authors
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Funding
Funding for this research was provided by:
National Defense Science and Technology Key Laboratory Fund (2020020056)
Foundation Strengthening Project (2019-JCJQ-JJ-077)
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Article History
Received: 7 March 2022
Revised: 24 December 2022
Accepted: 24 January 2023
First Online: 16 February 2023
Declarations
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: On behalf of all authors, the corresponding author states that there is no conflict of interest.
: For replication of the results, the shape data of the morphing wing at 20°-, 30°-, 70° sweep angle states are given and the optimization results are given. The experimental aerodynamic force coefficients of both the morphing and fixed wings at subsonic and supersonic conditions are given. The optimization code is not given here because of the copyright issues.
